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 48391U 26145.26270838 +.00000000 +00000-0 +37041-4 0 00001
2 48391 53.1612 336.8669 0001111 82.1171 277.9956 15.31698465 03
| Epoch (UTC): | 25 May 2026 06:18:18 |
| Eccentricity: | 0.0001111 |
| inclination: | 53.1612° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 336.8669° |
| argument of perigee: | 82.1171° |
| revolutions per day: | 15.31698465 |
| mean anomaly at epoch: | 277.9956° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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