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

PICO-02A021

In orbit NORAD 60538 EXCD-3754-5634-2238-2055

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

9

Observations all time

Mission information
Spacecraft name
PICO-02A021
Other names
PICO-1B-1
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 21:28:29
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
548.07 km
Apogee
554.31 km
Inclination
97.7°
Period
95.7 min
Semi-major axis
6929.3 km
Velocity
7.58 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:57 UTC
Two-line elements (TLE)
1 60538U 24149BY  26283.48638582  .00004140  00000-0  30294-3 0  9997
2 60538 97.6687 1.3408 0004422 6.6049 353.5234 15.04135176117063
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 02:22:09 ICEYE-X37
NORAD 59102
PICO-02A021
NORAD 60538
4.667 7.65 1.8e-07
2026-10-12 19:40:22 PICO-02A021
NORAD 60538
FENGYUN 1C DEB
NORAD 30912
2.717 14.99 2.2e-07
2026-10-14 06:56:28 PICO-02A021
NORAD 60538
COSMOS 886 DEB
NORAD 20673
4.778 14.42 8.7e-08
2026-10-15 09:02:06 RISAT-2B
NORAD 44233
PICO-02A021
NORAD 60538
3.228 7.67 3.7e-07
2026-10-16 01:24:12 PICO-02A021
NORAD 60538
NAXING 1
NORAD 28221
3.577 5.80 3.2e-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