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Sateliot 3

In orbit NORAD 60552 DBDL-2985-5402-8531-7144

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
Sateliot 3
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
2024-08-16 18:56:00
Separation time
2024-08-16 21:29:02
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
564.94 km
Apogee
572.68 km
Inclination
97.7°
Period
96.1 min
Semi-major axis
6946.9 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:57 UTC
Two-line elements (TLE)
1 60552U 24149CN  26283.20828068  .00001607  00000-0  13950-3 0  9998
2 60552 97.6723 358.0594 0005560 66.0072 294.1733 14.98416205117306
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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
2026-10-11 03:00:43 SATELIOT_3
NORAD 60552
DMSP 5D-3 F15 DEB
NORAD 26147
4.965 6.46 1.6e-07
2026-10-11 19:37:43 SATELIOT_3
NORAD 60552
STARLINK-36166
NORAD 67084
4.297 15.01 2.6e-06
2026-10-11 20:49:04 STARLINK-6036
NORAD 56800
SATELIOT_3
NORAD 60552
4.819 14.82 2.2e-06
2026-10-12 15:25:46 SATELIOT_3
NORAD 60552
DELTA 1 DEB
NORAD 26036
2.708 14.97 2.2e-07
2026-10-12 21:13:10 SATELIOT_3
NORAD 60552
STARLINK-36222
NORAD 67097
3.771 15.05 3.3e-06
2026-10-13 17:12:05 SATELIOT_3
NORAD 60552
STARLINK-35841
NORAD 67086
4.757 15.05 2.1e-06
2026-10-13 18:00:10 SATELIOT_3
NORAD 60552
STARLINK-35841
NORAD 67086
4.297 15.06 2.5e-06
2026-10-14 11:07:40 SATELIOT_3
NORAD 60552
NOAA 16 DEB
NORAD 41520
4.837 10.89 1.4e-07
2026-10-14 11:34:57 SATELIOT_3
NORAD 60552
STARLINK-36230
NORAD 67075
1.986 15.06 1.2e-05
2026-10-14 19:34:21 SATELIOT_3
NORAD 60552
STARLINK-36170
NORAD 67083
3.380 15.06 4.1e-06
2026-10-15 12:00:38 SATELIOT_3
NORAD 60552
BRO-15
NORAD 60553
4.335 0.22 2.3e-07
2026-10-15 14:31:23 STARLINK-5900
NORAD 55948
SATELIOT_3
NORAD 60552
3.573 8.80 8.7e-06
2026-10-15 18:31:46 STARLINK-5900
NORAD 55948
SATELIOT_3
NORAD 60552
4.490 8.76 5.6e-06
2026-10-15 20:07:56 STARLINK-5900
NORAD 55948
SATELIOT_3
NORAD 60552
3.961 8.74 7.1e-06
2026-10-15 23:37:07 SATELIOT_3
NORAD 60552
DEMOSAT/FALCON 1
NORAD 33393
1.641 10.58 1.2e-06
2026-10-16 09:44:46 STARLINK-3068
NORAD 49154
SATELIOT_3
NORAD 60552
4.434 9.62 5.4e-06
2026-10-16 12:50:21 SATELIOT_3
NORAD 60552
LEMUR-2-KRISH
NORAD 64561
2.372 5.05 7.4e-07
2026-10-16 14:34:03 STARLINK-5893
NORAD 55952
SATELIOT_3
NORAD 60552
4.069 8.46 6.9e-06
2026-10-16 16:10:14 STARLINK-5893
NORAD 55952
SATELIOT_3
NORAD 60552
4.951 8.44 4.6e-06
2026-10-16 20:10:37 STARLINK-5893
NORAD 55952
SATELIOT_3
NORAD 60552
2.517 8.40 1.8e-05
2026-10-16 22:09:50 SATELIOT_3
NORAD 60552
PEGASUS DEB
NORAD 24197
2.629 15.14 2.1e-07
2026-10-16 23:31:37 SATELIOT_3
NORAD 60552
STARLINK-36215
NORAD 67100
0.576 15.03 1.4e-04
2026-10-17 00:19:43 SATELIOT_3
NORAD 60552
STARLINK-36215
NORAD 67100
3.922 15.01 3.1e-06

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