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 data is extracted from the following two-line orbital elements,
1 48274U 21035A 23155.55269710 .00027573 00000-0 33792-3 0 9998
2 48274 41.4733 232.6562 0003765 295.6171 64.4279 15.59719635119865
| Epoch (UTC): | 04 June 2023 13:15:53 |
| Eccentricity: | 0.0003765 |
| inclination: | 41.4733° |
| perigee height: | 386 km |
| apogee height: | 391 km |
| right ascension of ascending node: | 232.6562° |
| argument of perigee: | 295.6171° |
| revolutions per day: | 15.59719635 |
| mean anomaly at epoch: | 64.4279° |
| orbit number at epoch: | 11986 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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