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 48798U 26145.29525183 +.00000000 +00000-0 +37805-4 0 00009
2 48798 87.8999 263.7497 0001398 99.4566 260.6722 13.15547038 08
| Epoch (UTC): | 25 May 2026 07:05:09 |
| Eccentricity: | 0.0001398 |
| inclination: | 87.8999° |
| perigee height: | 1201 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7497° |
| argument of perigee: | 99.4566° |
| revolutions per day: | 13.15547038 |
| mean anomaly at epoch: | 260.6722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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