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 42825U 26145.62312442 +.00000000 +00000-0 +93652-4 0 00005
2 42825 97.3597 51.6044 0001953 85.1875 274.9585 15.22859722 08
| Epoch (UTC): | 25 May 2026 14:57:17 |
| Eccentricity: | 0.0001953 |
| inclination: | 97.3597° |
| perigee height: | 496 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 51.6044° |
| argument of perigee: | 85.1875° |
| revolutions per day: | 15.22859722 |
| mean anomaly at epoch: | 274.9585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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