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 48797U 26145.35862351 +.00000000 +00000-0 -16100-3 0 00001
2 48797 87.8989 263.7558 0001933 104.2452 255.8893 13.15546577 00
| Epoch (UTC): | 25 May 2026 08:36:25 |
| Eccentricity: | 0.0001933 |
| inclination: | 87.8989° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7558° |
| argument of perigee: | 104.2452° |
| revolutions per day: | 13.15546577 |
| mean anomaly at epoch: | 255.8893° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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