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2024-105B

In orbit NORAD 59918 JSNX-1006-2190-3752-0693 China

2024

Launch

1

Observations all time

Mission information
Spacecraft name
2024-105B
Other names
2024-105B
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch time
2024-05-30 00:00:00
Separation time
2024-05-30 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
494.02 km
Apogee
509.70 km
Inclination
97.6°
Period
94.7 min
Semi-major axis
6880.0 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 13:08:39 UTC
Two-line elements (TLE)
1 59918U 24105B   26285.34594124  .00005400  00000-0  25120-3 0  9991
2 59918 97.5778 301.3375 0011509 189.4322 170.6698 15.20327341130845
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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
2026-10-13 07:35:20 OBJECT B
NORAD 59918
FENGYUN 1C DEB
NORAD 32464
4.917 0.62 1.8e-07
2026-10-13 21:47:49 OBJECT B
NORAD 59918
YAOGAN-1 DEB
NORAD 36365
3.034 7.54 4.2e-07
2026-10-14 04:07:15 OBJECT B
NORAD 59918
OBJECT D
NORAD 66056
3.376 6.37 3.6e-07
2026-10-14 08:04:16 OBJECT B
NORAD 59918
OBJECT D
NORAD 66056
3.190 6.38 4.0e-07
2026-10-15 02:19:56 OBJECT B
NORAD 59918
LPNTSAT-001 (IOD-1)
NORAD 68408
3.881 14.07 1.4e-07
2026-10-15 19:43:07 STARLINK-4624
NORAD 53684
OBJECT B
NORAD 59918
3.574 14.30 4.8e-06
2026-10-16 09:19:24 OBJECT B
NORAD 59918
SL-3 R/B
NORAD 12904
4.137 2.46 7.0e-07
2026-10-16 12:48:00 OBJECT B
NORAD 59918
TOMORROW-S8
NORAD 66308
4.844 12.71 1.2e-07
2026-10-16 19:20:12 OBJECT B
NORAD 59918
IRIDE-MS1-EAGLET 2-11
NORAD 68453
3.728 7.41 2.8e-07
2026-10-16 20:54:58 OBJECT B
NORAD 59918
IRIDE-MS1-EAGLET 2-11
NORAD 68453
1.811 7.41 1.2e-06
2026-10-16 22:29:45 OBJECT B
NORAD 59918
IRIDE-MS1-EAGLET 2-11
NORAD 68453
1.007 7.41 3.9e-06
2026-10-17 00:04:31 OBJECT B
NORAD 59918
IRIDE-MS1-EAGLET 2-11
NORAD 68453
2.623 7.41 5.7e-07
2026-10-17 01:39:18 OBJECT B
NORAD 59918
IRIDE-MS1-EAGLET 2-11
NORAD 68453
4.546 7.41 1.9e-07
2026-10-17 17:24:56 OBJECT B
NORAD 59918
PIAST-S2
NORAD 66757
4.960 7.06 1.6e-07
2026-10-17 18:14:28 OBJECT B
NORAD 59918
IRIDE-MS1-EAGLET 2-11
NORAD 68453
4.982 7.43 1.6e-07
2026-10-17 18:29:09 OBJECT B
NORAD 59918
SPACEMOBILE-002
NORAD 61048
4.995 14.53 7.8e-08
2026-10-17 19:49:15 OBJECT B
NORAD 59918
IRIDE-MS1-EAGLET 2-11
NORAD 68453
3.388 7.43 3.4e-07
2026-10-17 21:24:01 OBJECT B
NORAD 59918
IRIDE-MS1-EAGLET 2-11
NORAD 68453
2.178 7.43 8.3e-07
2026-10-17 22:58:48 OBJECT B
NORAD 59918
IRIDE-MS1-EAGLET 2-11
NORAD 68453
2.104 7.43 8.9e-07
2026-10-18 00:33:34 OBJECT B
NORAD 59918
IRIDE-MS1-EAGLET 2-11
NORAD 68453
3.216 7.43 3.8e-07
2026-10-18 01:40:52 YAOGAN-39 04B
NORAD 58143
OBJECT B
NORAD 59918
2.035 8.06 9.2e-07
2026-10-18 02:08:21 OBJECT B
NORAD 59918
IRIDE-MS1-EAGLET 2-11
NORAD 68453
4.723 7.43 1.8e-07
2026-10-18 06:12:03 OBJECT B
NORAD 59918
STPSAT-7
NORAD 68630
2.840 13.01 3.2e-07
2026-10-18 08:25:23 OBJECT B
NORAD 59918
OBJECT E
NORAD 61231
4.917 6.83 1.7e-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