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 48225U 26145.40311664 +.00000000 +00000-0 +68181-3 0 00004
2 48225 87.8944 294.2468 0002118 100.3487 259.7882 13.14501192 01
| Epoch (UTC): | 25 May 2026 09:40:29 |
| Eccentricity: | 0.0002118 |
| inclination: | 87.8944° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2468° |
| argument of perigee: | 100.3487° |
| revolutions per day: | 13.14501192 |
| mean anomaly at epoch: | 259.7882° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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