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 48061U 26145.49849014 +.00000000 +00000-0 +48031-3 0 00008
2 48061 87.8944 324.7398 0001608 100.0026 260.1285 13.13468800 09
| Epoch (UTC): | 25 May 2026 11:57:49 |
| Eccentricity: | 0.0001608 |
| inclination: | 87.8944° |
| perigee height: | 1209 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7398° |
| argument of perigee: | 100.0026° |
| revolutions per day: | 13.13468800 |
| mean anomaly at epoch: | 260.1285° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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