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 22825U 26161.42702727 +.00000000 +00000-0 +45162-4 0 00001
2 22825 98.6881 228.8428 0009436 117.2772 242.9373 14.30940455 09
| Epoch (UTC): | 10 June 2026 10:14:55 |
| Eccentricity: | 0.0009436 |
| inclination: | 98.6881° |
| perigee height: | 782 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 228.8428° |
| argument of perigee: | 117.2772° |
| revolutions per day: | 14.30940455 |
| mean anomaly at epoch: | 242.9373° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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