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MAGNARO-II - Piscis

In orbit NORAD 68798 CFXV-4372-6054-0301-8168

Time in UTC

11:02

Next pass · Чукотка · 10°

11.10 12:45

Scheduled · JHR

105

Observations over 30 days

71%

Successful observations

1k

Frames, latest 2026-10-10 12:59 UTC

Mission information
Spacecraft name
MAGNARO-II - Piscis
Call sign
JJ2YXG
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Electron
Spaceport
Rocket Lab Launch Complex 1A
Launch time
2026-04-23 03:09:00
Separation time
Last observers
Observer
Time of receipt
2026-10-10 12:57:57 UTC
2026-10-10 12:59:49 UTC
2026-10-09 23:58:31 UTC
2026-10-09 14:46:40 UTC
2026-10-09 01:45:31 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
521.07 km
Apogee
548.55 km
Inclination
97.5°
Period
95.4 min
Semi-major axis
6912.9 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:21 UTC
Two-line elements (TLE)
1 68798U 26088G   26282.85521641  .00002865  00000-0  18209-3 0  9998
2 68798 97.5229 69.9137 0019872 51.1880 309.1119 15.09468093 25599
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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 02:22:49 DUBAISAT-2
NORAD 39419
MAGNARO-II
NORAD 68798
1.550 14.80 7.2e-07
2026-10-16 00:04:19 MAGNARO-II
NORAD 68798
PEGASUS DEB
NORAD 39319
2.650 14.85 2.5e-07
2026-10-16 04:28:45 MAGNARO-II
NORAD 68798
MINOTAUR 4 DEB
NORAD 52037
3.685 5.64 3.0e-07
2026-10-16 15:13:19 OBJECT G
NORAD 68204
MAGNARO-II
NORAD 68798
3.402 9.04 3.2e-07
2026-10-17 00:32:33 STARLINK-3177
NORAD 51138
MAGNARO-II
NORAD 68798
4.298 8.39 6.2e-06
2026-10-17 02:19:32 OBJECT D
NORAD 62732
MAGNARO-II
NORAD 68798
1.034 2.97 4.1e-06
2026-10-17 05:26:37 MAGNARO-II
NORAD 68798
METEOR 2-5 DEB
NORAD 38275
2.796 15.19 1.9e-07
2026-10-17 07:02:01 MAGNARO-II
NORAD 68798
METEOR 2-5 DEB
NORAD 38275
1.633 15.19 5.6e-07
2026-10-17 08:27:51 STARLINK-5054
NORAD 53906
MAGNARO-II
NORAD 68798
3.340 7.34 1.1e-05
2026-10-17 08:37:26 MAGNARO-II
NORAD 68798
METEOR 2-5 DEB
NORAD 38275
3.386 15.19 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