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 26150.61688937 +.00000000 +00000-0 +13669-3 0 00004
2 42825 97.3599 56.4977 0001909 84.2730 275.8724 15.22890007 05
| Epoch (UTC): | 30 May 2026 14:48:19 |
| Eccentricity: | 0.0001909 |
| inclination: | 97.3599° |
| perigee height: | 496 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 56.4977° |
| argument of perigee: | 84.2730° |
| revolutions per day: | 15.22890007 |
| mean anomaly at epoch: | 275.8724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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