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 21799U 91076C 23264.13482161 0.00004100 00000-0 46306-3 0 04
2 21799 63.3066 285.2639 0900659 56.9878 303.0122 13.45518148 02
| Epoch (UTC): | 21 September 2023 03:14:08 |
| Eccentricity: | 0.0900659 |
| inclination: | 63.3066° |
| perigee height: | 416 km |
| apogee height: | 1761 km |
| right ascension of ascending node: | 285.2639° |
| argument of perigee: | 56.9878° |
| revolutions per day: | 13.45518148 |
| mean anomaly at epoch: | 303.0122° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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