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 23036.80809352 .00013505 00000-0 15923-3 0 9992
2 48274 41.4739 236.9695 0002646 162.0632 312.4988 15.61111010101287
| Epoch (UTC): | 05 February 2023 19:23:39 |
| Eccentricity: | 0.0002646 |
| inclination: | 41.4739° |
| perigee height: | 382 km |
| apogee height: | 386 km |
| right ascension of ascending node: | 236.9695° |
| argument of perigee: | 162.0632° |
| revolutions per day: | 15.61111010 |
| mean anomaly at epoch: | 312.4988° |
| orbit number at epoch: | 10128 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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