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PELICAN-5

In orbit NORAD 66667 RBKD-9742-1904-9336-8150

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
PELICAN-5
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
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
447.91 km
Apogee
451.90 km
Inclination
97.4°
Period
93.6 min
Semi-major axis
6828.0 km
Velocity
7.64 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-09 12:46:41 UTC
Two-line elements (TLE)
1 66667U 25276B   26282.01939698  .00027776  00000-0  75109-3 0  9992
2 66667 97.3591 357.3030 0002922 122.9813 237.1713 15.37680982 47979
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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 00:23:22 PELICAN-5
NORAD 66667
KUIPER-00540
NORAD 69609
2.065 14.65 4.4e-07
2026-10-12 06:20:41 STARLINK-3540
NORAD 51719
PELICAN-5
NORAD 66667
3.810 9.02 7.6e-06
2026-10-12 12:42:22 LONGJIANG 3
NORAD 56874
PELICAN-5
NORAD 66667
2.509 14.50 3.1e-07
2026-10-12 22:03:35 STARLINK-3725
NORAD 52123
PELICAN-5
NORAD 66667
4.095 14.63 3.4e-06
2026-10-13 08:39:29 PELICAN-5
NORAD 66667
CZ-6A DEB
NORAD 54413
1.350 12.12 1.6e-06
2026-10-13 21:10:33 GEISAT PRECURSOR
NORAD 56934
PELICAN-5
NORAD 66667
2.034 8.65 9.0e-07
2026-10-13 23:01:17 PELICAN-5
NORAD 66667
STARLINK-37439
NORAD 69377
3.960 6.72 7.7e-06
2026-10-14 11:24:39 STARLINK-4197
NORAD 52849
PELICAN-5
NORAD 66667
4.424 12.08 4.5e-06
2026-10-14 12:49:59 PELICAN-5
NORAD 66667
FENGYUN 1C DEB
NORAD 47041
2.954 2.06 5.0e-07
2026-10-14 21:21:41 PELICAN-5
NORAD 66667
CZ-6A DEB
NORAD 58433
1.346 11.29 1.7e-06
2026-10-15 00:24:16 PELICAN-5
NORAD 66667
FENGYUN 1C DEB
NORAD 30520
1.565 14.65 7.8e-07
2026-10-15 07:00:20 PELICAN-5
NORAD 66667
SSC
NORAD 13874
4.040 5.65 2.5e-07
2026-10-15 10:57:26 STARLINK-4275
NORAD 53008
PELICAN-5
NORAD 66667
4.666 14.63 2.6e-06
2026-10-15 21:35:55 PELICAN-5
NORAD 66667
COSMOS 807
NORAD 8744
2.628 14.82 5.4e-07
2026-10-16 15:09:37 PELICAN-5
NORAD 66667
STARLINK-38011
NORAD 100412
4.628 14.77 2.6e-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