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 48068U 26145.21238457 +.00000000 +00000-0 -64820-3 0 00003
2 48068 87.8950 324.7961 0001735 97.4266 262.7060 13.13468506 07
| Epoch (UTC): | 25 May 2026 05:05:50 |
| Eccentricity: | 0.0001735 |
| inclination: | 87.8950° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7961° |
| argument of perigee: | 97.4266° |
| revolutions per day: | 13.13468506 |
| mean anomaly at epoch: | 262.7060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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