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 28895U 05043F 23332.90165571 .00003419 00000-0 62527-3 0 9993
2 28895 98.1758 104.0094 0015001 273.1756 86.7731 14.66470520964947
| Epoch (UTC): | 28 November 2023 21:38:23 |
| Eccentricity: | 0.0015001 |
| inclination: | 98.1758° |
| perigee height: | 662 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 104.0094° |
| argument of perigee: | 273.1756° |
| revolutions per day: | 14.66470520 |
| mean anomaly at epoch: | 86.7731° |
| orbit number at epoch: | 96494 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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