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 48283U 26145.59113420 +.00000000 +00000-0 +12621-3 0 00006
2 48283 53.1594 77.6995 0001477 92.3549 267.7621 15.31698511 09
| Epoch (UTC): | 25 May 2026 14:11:13 |
| Eccentricity: | 0.0001477 |
| inclination: | 53.1594° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 77.6995° |
| argument of perigee: | 92.3549° |
| revolutions per day: | 15.31698511 |
| mean anomaly at epoch: | 267.7621° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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