View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 61056U 26145.38524808 +.00000000 +00000-0 +10071-4 0 00000
2 61056 53.1588 292.5336 0000860 64.2145 295.8961 15.68837968 07
| Epoch (UTC): | 25 May 2026 09:14:45 |
| Eccentricity: | 0.0000860 |
| inclination: | 53.1588° |
| perigee height: | 362 km |
| apogee height: | 363 km |
| right ascension of ascending node: | 292.5336° |
| argument of perigee: | 64.2145° |
| revolutions per day: | 15.68837968 |
| mean anomaly at epoch: | 295.8961° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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