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 28537U 05004A 23142.16722996 0.00000000 00000-0 00000-0 0 01
2 28537 63.4106 60.8588 0457777 0.4079 359.6262 13.40871753 01
| Epoch (UTC): | 22 May 2023 04:00:48 |
| Eccentricity: | 0.0457777 |
| inclination: | 63.4106° |
| perigee height: | 763 km |
| apogee height: | 1448 km |
| right ascension of ascending node: | 60.8588° |
| argument of perigee: | 0.4079° |
| revolutions per day: | 13.40871753 |
| mean anomaly at epoch: | 359.6262° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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