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SAL-E

In orbit NORAD 68458 WKBS-6047-7369-7033-9398 United States of America

Time in UTC

11.10 11:58

Scheduled · Геоскан

114

Observations over 30 days

53%

Successful observations

7k

Frames, latest 2026-10-11 02:46 UTC

Mission information
Spacecraft name
SAL-E
Other names
CP16
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
Separation time
Last observers
Observer
Time of receipt
2026-10-11 02:46:05 UTC
2026-10-11 01:17:42 UTC
2026-10-11 01:14:57 UTC
2026-10-10 12:21:45 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
500.40 km
Apogee
510.12 km
Inclination
97.5°
Period
94.8 min
Semi-major axis
6883.4 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:40 UTC
Two-line elements (TLE)
1 68458U 26067AU  26283.70082494  .00008232  00000-0  39415-3 0  9997
2 68458 97.4624 240.3577 0007064 46.1193 314.0624 15.19188136 29468
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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
2026-10-12 08:43:50 FEMTO-1
NORAD 68419
SAL-E
NORAD 68458
1.746 0.06 1.4e-06
2026-10-12 10:17:43 OBJECT B
NORAD 59918
SAL-E
NORAD 68458
3.140 7.47 4.0e-07
2026-10-12 16:35:11 OBJECT AE
NORAD 67276
SAL-E
NORAD 68458
4.828 12.80 1.2e-07
2026-10-13 00:29:28 NUSAT-47
NORAD 66743
SAL-E
NORAD 68458
3.697 12.74 2.0e-07
2026-10-13 01:42:55 SAL-E
NORAD 68458
SL-24 R/B
NORAD 31699
3.029 0.13 1.9e-07
2026-10-13 02:03:05 SAL-E
NORAD 68458
CZ-6A DEB
NORAD 54307
4.727 13.54 1.1e-07
2026-10-13 06:01:45 OBJECT D
NORAD 66056
SAL-E
NORAD 68458
4.705 12.29 1.3e-07
2026-10-13 06:49:09 OBJECT D
NORAD 66056
SAL-E
NORAD 68458
2.655 12.32 4.0e-07
2026-10-13 14:47:48 STARLINK-4570
NORAD 53690
SAL-E
NORAD 68458
4.336 10.10 5.5e-06
2026-10-14 15:11:31 SAL-E
NORAD 68458
COSMOS 2251 DEB
NORAD 36551
4.958 14.53 7.8e-08
2026-10-14 19:50:19 STARLINK-3107
NORAD 49171
SAL-E
NORAD 68458
2.767 14.95 6.5e-06
2026-10-15 02:19:14 SAL-E
NORAD 68458
OKEAN-2
NORAD 20510
0.927 13.78 3.5e-05
2026-10-16 07:32:12 GAOFEN-7
NORAD 44703
SAL-E
NORAD 68458
3.740 11.94 2.1e-07
2026-10-16 13:46:08 DB SKYFORGE CORE TU
NORAD 68445
SAL-E
NORAD 68458
4.810 0.00 1.7e-07
2026-10-16 16:19:15 SAL-E
NORAD 68458
ELECTRON KICK STAGE R/B
NORAD 45728
4.019 12.28 1.8e-07
2026-10-17 02:32:42 SPOQC
NORAD 68423
SAL-E
NORAD 68458
0.610 0.05 1.2e-05
2026-10-17 02:47:41 SAL-E
NORAD 68458
COSMOS 2251 DEB
NORAD 36047
1.431 15.16 7.4e-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