Luna E-6 No.2

soviet lunar lander that failed to achieve planned orbit
Vehicle space_probe Q2249850

Facts

17 properties
Instance of
space probe
Followed by
Luna E-6 No.3[3]
Launch date
1963-01-04
Part of the series
Luna programme[4]
Apoapsis
151 km[14]
Launch vehicle
Molniya
Mass
2,500 kg[12]
Orbital inclination
64.9 degree[11]
Orbital period
87.5 minute[13]
Part of series
Luna programme
Periapsis
151 km[15]
Space launch vehicle
Molniya[5]
Time of object orbit decay
January 5, 1963[7]
UTC date of spacecraft launch
January 4, 1963[6]
🏷️ Also known as
en Luna E-6 No.2 hu Luna E–6–1 it Sputnik 25 ja スプートニク25号 nl Spoetnik 25 ru Е-6 № 2 ru Луна-4C ru Спутник-25
🔖 Identifiers · 5
COSPAR ID
1963-001A
Freebase ID
/m/0lb7l
NSSDCA ID
1963-001A

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🔗 Connections
Significant event 2
Followed by 1
Followed by (predecessor) 1
Follows 1
Instance of 1
Part of the series 1
Preceded by (successor) 1
Space launch vehicle 1
Start point 1
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Summary

Luna E-6 No.2 is a space probe[1].

📑 Cite this page

Use these citations when quoting this entity in research, articles, AI prompts, or wherever provenance matters. We aggregate Wikidata + Wikipedia + authoritative open-data sources; the stitched, scored, cross-referenced view is what 4ort.xyz contributes.

APA 4ort.xyz Knowledge Graph. (2026). Luna E-6 No.2. Retrieved November 3, 2026, from https://4ort.xyz/entity/luna-e-6-no-2
MLA “Luna E-6 No.2.” 4ort.xyz Knowledge Graph, 4ort.xyz, 3 Nov. 2026, https://4ort.xyz/entity/luna-e-6-no-2.
BibTeX @misc{4ortxyz_luna-e-6-no-2_2026, author = {{4ort.xyz Knowledge Graph}}, title = {{Luna E-6 No.2}}, year = {2026}, url = {https://4ort.xyz/entity/luna-e-6-no-2}, note = {Accessed: 2026-11-03}}
LLM prompt According to 4ort.xyz Knowledge Graph (aggregator of Wikidata, Wikipedia, and authoritative open-data sources): Luna E-6 No.2 — https://4ort.xyz/entity/luna-e-6-no-2 (retrieved 2026-11-03)

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