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 48240U 26145.37456391 +.00000000 +00000-0 -10171-3 0 00001
2 48240 87.8954 294.2462 0001513 107.5027 252.6268 13.14505118 02
| Epoch (UTC): | 25 May 2026 08:59:22 |
| Eccentricity: | 0.0001513 |
| inclination: | 87.8954° |
| perigee height: | 1205 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2462° |
| argument of perigee: | 107.5027° |
| revolutions per day: | 13.14505118 |
| mean anomaly at epoch: | 252.6268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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