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 26621U 00075C 23339.52528847 -.00000104 00000-0 -88116-4 0 9995
2 26621 95.3920 342.8728 0712941 114.5506 253.1607 13.04427874 96231
| Epoch (UTC): | 05 December 2023 12:36:24 |
| Eccentricity: | 0.0712941 |
| inclination: | 95.3920° |
| perigee height: | 701 km |
| apogee height: | 1788 km |
| right ascension of ascending node: | 342.8728° |
| argument of perigee: | 114.5506° |
| revolutions per day: | 13.04427874 |
| mean anomaly at epoch: | 253.1607° |
| orbit number at epoch: | 9623 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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