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

ORESAT0.5

In orbit NORAD 60525 DKCD-1609-0567-7056-3922 United States of America

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

33

Observations all time

Mission information
Spacecraft name
ORESAT0.5
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
2024-08-16 18:56:00
Separation time
2024-08-16 19:53:18
Last observers
Observer
Time of receipt
2024-08-18 19:38:59 UTC
2024-08-18 10:24:19 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
412.72 km
Apogee
418.92 km
Inclination
97.4°
Period
92.9 min
Semi-major axis
6793.8 km
Velocity
7.64 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:44 UTC
Two-line elements (TLE)
1 60525U 24149BK  26284.21206953  .00030926  00000-0  56555-3 0  9997
2 60525 97.3680 12.3045 0004573 201.4018 158.7043 15.49307167120412
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 13:37:01 STARLINK-5704
NORAD 55486
ORESAT0.5
NORAD 60525
0.930 14.39 7.1e-05
2026-10-12 20:58:51 TIGER-7
NORAD 59141
ORESAT0.5
NORAD 60525
2.593 8.53 5.6e-07
2026-10-13 16:17:06 ORESAT0.5
NORAD 60525
OBJECT AS
NORAD 61775
4.861 14.48 8.5e-08
2026-10-14 03:30:42 STARLINK-1296
NORAD 45412
ORESAT0.5
NORAD 60525
2.849 14.70 7.0e-06
2026-10-14 14:40:45 STARLINK-1153
NORAD 45080
ORESAT0.5
NORAD 60525
3.125 9.63 1.1e-05

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