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 24797U 97020F 23334.23008120 .00001854 00000-0 38296-3 0 9997
2 24797 86.9001 209.7022 0222051 15.1214 100.4770 14.45443274398156
| Epoch (UTC): | 30 November 2023 05:31:19 |
| Eccentricity: | 0.0222051 |
| inclination: | 86.9001° |
| perigee height: | 582 km |
| apogee height: | 898 km |
| right ascension of ascending node: | 209.7022° |
| argument of perigee: | 15.1214° |
| revolutions per day: | 14.45443274 |
| mean anomaly at epoch: | 100.4770° |
| orbit number at epoch: | 39815 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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