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 26486U 00051D 23264.99808007 .00000010 00000-0 00000-0 0 9991
2 26486 63.1264 306.7908 7377715 276.6406 253.7943 1.45765278122677
| Epoch (UTC): | 21 September 2023 23:57:14 |
| Eccentricity: | 0.7377715 |
| inclination: | 63.1264° |
| perigee height: | 2238 km |
| apogee height: | 50720 km |
| right ascension of ascending node: | 306.7908° |
| argument of perigee: | 276.6406° |
| revolutions per day: | 1.45765278 |
| mean anomaly at epoch: | 253.7943° |
| orbit number at epoch: | 12267 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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