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 48908U 26066.49507354 +.00000000 +00000-0 +59128-3 0 00007
2 48908 97.7027 251.0779 0003816 9.6606 350.4719 15.54222114 05
| Epoch (UTC): | 07 March 2026 11:52:54 |
| Eccentricity: | 0.0003816 |
| inclination: | 97.7027° |
| perigee height: | 402 km |
| apogee height: | 407 km |
| right ascension of ascending node: | 251.0779° |
| argument of perigee: | 9.6606° |
| revolutions per day: | 15.54222114 |
| mean anomaly at epoch: | 350.4719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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