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 55978U 26145.65114178 +.00000000 +00000-0 +13624-3 0 00007
2 55978 97.5889 71.5004 0002271 113.8901 246.2574 15.24717545 05
| Epoch (UTC): | 25 May 2026 15:37:38 |
| Eccentricity: | 0.0002271 |
| inclination: | 97.5889° |
| perigee height: | 490 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 71.5004° |
| argument of perigee: | 113.8901° |
| revolutions per day: | 15.24717545 |
| mean anomaly at epoch: | 246.2574° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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