RU | EN | ZH --:-- UTC Sign in
Back

PANDORA

In orbit NORAD 67395 WNBO-7941-4526-5543-5786

Observations 0
Go to map
Back

2026

Falcon 9 Block 5 | Pandora / Twilight rideshare mission

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
PANDORA
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch
Falcon 9 Block 5 | Pandora / Twilight rideshare mission
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2026-01-11 13:18:59
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
595.85 km
Apogee
605.16 km
Inclination
97.8°
Period
96.8 min
Semi-major axis
6978.6 km
Velocity
7.55 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:40 UTC
Two-line elements (TLE)
1 67395U 26004AJ  26283.95505424  .00000638  00000-0  75033-4 0  9996
2 67395  97.8118 280.8742 0006673 103.8771 256.3189 14.88225652 40490
Copy content
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 08:28:00 PANDORA
NORAD 67395 		COSMOS 2251 DEB
NORAD 34681 		2.366 13.41 4.3e-07
2026-10-12 09:53:33 PANDORA
NORAD 67395 		SL-14 R/B
NORAD 11672 		4.811 15.08 1.5e-07
2026-10-12 10:04:49 PANDORA
NORAD 67395 		COSMOS 2251 DEB
NORAD 34681 		4.824 13.40 1.0e-07
2026-10-13 01:18:11 PANDORA
NORAD 67395 		COSMOS 2535 DEB
NORAD 44712 		2.795 0.10 5.6e-07
2026-10-13 01:25:24 PANDORA
NORAD 67395 		NOAA 16 DEB
NORAD 42379 		1.060 13.49 2.1e-06
2026-10-13 02:07:19 PANDORA
NORAD 67395 		CZ-6A DEB
NORAD 54929 		3.483 9.32 3.0e-07
2026-10-13 23:40:40 PANDORA
NORAD 67395 		COSMOS 2251 DEB
NORAD 34412 		3.405 15.14 1.3e-07
2026-10-15 15:05:58 GEESAT-6 01
NORAD 65713 		PANDORA
NORAD 67395 		3.917 14.51 1.2e-07
2026-10-17 20:30:23 GEESAT-3 03
NORAD 61013 		PANDORA
NORAD 67395 		3.273 8.60 3.5e-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