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 28054U 03048A 23088.54596619 .00000352 00000-0 21020-3 0 9998
2 28054 99.0112 86.1485 0006446 226.7314 241.6086 14.13782617 3303
| Epoch (UTC): | 29 March 2023 13:06:11 |
| Eccentricity: | 0.0006446 |
| inclination: | 99.0112° |
| perigee height: | 842 km |
| apogee height: | 851 km |
| right ascension of ascending node: | 86.1485° |
| argument of perigee: | 226.7314° |
| revolutions per day: | 14.13782617 |
| mean anomaly at epoch: | 241.6086° |
| orbit number at epoch: | 330 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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