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

Iperdrone.0

In orbit NORAD 60520 EBRB-9167-1241-1151-0289

Time in UTC

12:02

Next pass · Обозерский · 12°

13.10 20:48

Scheduled · ЦМИТ ГЕНЕЗИС

76

Observations over 30 days

24%

Successful observations

94k

Frames, latest 2026-10-12 10:42 UTC

Mission information
Spacecraft name
Iperdrone.0
Other names
TYVAK-0415
Status
Active
The satellite is in orbit
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 19:54:43
Last observers
Observer
Time of receipt
2026-10-12 10:42:05 UTC
2026-10-09 10:40:52 UTC
2026-10-06 10:31:50 UTC
2026-09-22 10:15:01 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
261.47 km
Apogee
268.14 km
Inclination
97.4°
Period
89.8 min
Semi-major axis
6641.0 km
Velocity
7.74 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-13 06:09:03 UTC
Two-line elements (TLE)
1 60520U 24149BE  26285.79834168  .00574604  15511-3  95240-3 0  9997
2 60520 97.3617 27.0057 0004796 243.1096 116.9694 16.03051884121477
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
2026-10-16 03:33:44 IPERDRONE.0
NORAD 60520
RASSVET-3 23
NORAD 100089
4.933 11.86 1.3e-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