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 42954U 26145.62355645 +.00000000 +00000-0 +12220-3 0 00001
2 42954 97.6530 184.3659 0017194 168.4146 191.7466 14.81151460 09
| Epoch (UTC): | 25 May 2026 14:57:55 |
| Eccentricity: | 0.0017194 |
| inclination: | 97.6530° |
| perigee height: | 614 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 184.3659° |
| argument of perigee: | 168.4146° |
| revolutions per day: | 14.81151460 |
| mean anomaly at epoch: | 191.7466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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