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 28654U 05018A 23335.17909461 .00000415 00000-0 24574-3 0 9997
2 28654 98.8958 48.6483 0013335 266.6214 93.3433 14.13068239955156
| Epoch (UTC): | 01 December 2023 04:17:53 |
| Eccentricity: | 0.0013335 |
| inclination: | 98.8958° |
| perigee height: | 839 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 48.6483° |
| argument of perigee: | 266.6214° |
| revolutions per day: | 14.13068239 |
| mean anomaly at epoch: | 93.3433° |
| orbit number at epoch: | 95515 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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