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 23340.33876831 .00002119 00000-0 39048-3 0 9995
2 28895 98.1753 111.4193 0015063 248.0120 111.9484 14.66520068966039
| Epoch (UTC): | 06 December 2023 08:07:49 |
| Eccentricity: | 0.0015063 |
| inclination: | 98.1753° |
| perigee height: | 661 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 111.4193° |
| argument of perigee: | 248.0120° |
| revolutions per day: | 14.66520068 |
| mean anomaly at epoch: | 111.9484° |
| orbit number at epoch: | 96603 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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