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LUNA-2

In orbit NORAD 68470 IMHH-4032-1798-6391-5710

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

59

Observations all time

Mission information
Spacecraft name
LUNA-2
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2026-03-30 11:02:00
Separation time
Last observers
Observer
Time of receipt
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
501.63 km
Apogee
512.32 km
Inclination
97.5°
Period
94.8 min
Semi-major axis
6885.1 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 68470U 26067BG  26287.10934213  .00005512  00000-0  26937-3 0  9997
2 68470 97.4637 243.6090 0007767 30.1399 330.0280 15.18622059 29971
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-15 11:11:33 OBJECT B
NORAD 65260
LUNA-2
NORAD 68470
4.624 15.01 7.5e-08
2026-10-15 14:21:22 OBJECT C
NORAD 65261
LUNA-2
NORAD 68470
3.179 15.00 1.6e-07
2026-10-15 15:56:12 OBJECT D
NORAD 65262
LUNA-2
NORAD 68470
1.997 15.01 4.0e-07
2026-10-16 01:37:44 CARTOSAT-3
NORAD 44804
LUNA-2
NORAD 68470
4.290 11.80 1.6e-07
2026-10-16 10:58:16 STARLINK-2112
NORAD 47391
LUNA-2
NORAD 68470
1.992 13.71 1.8e-05
2026-10-16 11:51:55 STARLINK-6061
NORAD 56795
LUNA-2
NORAD 68470
3.873 13.21 5.1e-06
2026-10-17 17:09:10 LUNA-2
NORAD 68470
FENGYUN 1C DEB
NORAD 31327
3.716 12.11 2.1e-07
2026-10-17 17:09:52 CARTOSAT-2D
NORAD 41948
LUNA-2
NORAD 68470
2.918 11.58 3.6e-07
2026-10-17 19:32:10 CARTOSAT-2D
NORAD 41948
LUNA-2
NORAD 68470
2.541 11.61 4.8e-07
2026-10-18 04:15:05 SJ-12
NORAD 36596
LUNA-2
NORAD 68470
4.699 8.00 1.7e-07
2026-10-18 06:06:12 YAOGAN-39 04C
NORAD 58145
LUNA-2
NORAD 68470
4.781 10.49 1.5e-07
2026-10-18 11:38:16 YAOGAN-39 04C
NORAD 58145
LUNA-2
NORAD 68470
2.840 10.41 4.2e-07
2026-10-19 01:29:44 LUNA-2
NORAD 68470
COSMOS 2251 DEB
NORAD 40794
4.154 6.38 2.3e-07
2026-10-19 07:42:56 STARLINK-5925
NORAD 55945
LUNA-2
NORAD 68470
1.366 15.08 2.6e-05
2026-10-19 14:51:04 LUNA-2
NORAD 68470
COSMOS 886 DEB
NORAD 18907
3.255 15.19 1.6e-07
2026-10-20 23:09:52 STARLINK-5862
NORAD 55920
LUNA-2
NORAD 68470
1.072 15.13 4.1e-05
2026-10-20 23:25:28 FOSSASAT-2E18 (TAT-A)
NORAD 62686
LUNA-2
NORAD 68470
4.442 13.05 1.3e-07

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite