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 42845U 26145.06625892 +.00000000 +00000-0 +77209-3 0 00000
2 42845 97.3624 336.2468 0004506 105.6802 254.4946 15.48047556 04
| Epoch (UTC): | 25 May 2026 01:35:24 |
| Eccentricity: | 0.0004506 |
| inclination: | 97.3624° |
| perigee height: | 419 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 336.2468° |
| argument of perigee: | 105.6802° |
| revolutions per day: | 15.48047556 |
| mean anomaly at epoch: | 254.4946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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