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 28366U 04025A 23084.12706054 .00000520 00000-0 17800-3 0 9994
2 28366 98.1284 303.3506 0106624 209.9700 149.5357 14.36961759982122
| Epoch (UTC): | 25 March 2023 03:02:58 |
| Eccentricity: | 0.0106624 |
| inclination: | 98.1284° |
| perigee height: | 692 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 303.3506° |
| argument of perigee: | 209.9700° |
| revolutions per day: | 14.36961759 |
| mean anomaly at epoch: | 149.5357° |
| orbit number at epoch: | 98212 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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