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 48907U 26145.25768279 +.00000000 +00000-0 +33446-3 0 00008
2 48907 97.7045 333.3112 0006213 82.3267 277.8691 15.53949067 07
| Epoch (UTC): | 25 May 2026 06:11:03 |
| Eccentricity: | 0.0006213 |
| inclination: | 97.7045° |
| perigee height: | 401 km |
| apogee height: | 409 km |
| right ascension of ascending node: | 333.3112° |
| argument of perigee: | 82.3267° |
| revolutions per day: | 15.53949067 |
| mean anomaly at epoch: | 277.8691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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