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 61054U 26145.42339786 +.00000000 +00000-0 -11255-4 0 00008
2 61054 53.1594 292.7899 0000788 59.3740 300.7355 15.69725331 07
| Epoch (UTC): | 25 May 2026 10:09:41 |
| Eccentricity: | 0.0000788 |
| inclination: | 53.1594° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 292.7899° |
| argument of perigee: | 59.3740° |
| revolutions per day: | 15.69725331 |
| mean anomaly at epoch: | 300.7355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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