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 00202U 61031A 24251.74342788 .00000197 00000-0 21151-3 0 9992
2 00202 32.4398 5.0506 0101414 336.7956 22.8108 13.63688283132567
| Epoch (UTC): | 07 September 2024 17:50:32 |
| Eccentricity: | 0.0101414 |
| inclination: | 32.4398° |
| perigee height: | 947 km |
| apogee height: | 1097 km |
| right ascension of ascending node: | 5.0506° |
| argument of perigee: | 336.7956° |
| revolutions per day: | 13.63688283 |
| mean anomaly at epoch: | 22.8108° |
| orbit number at epoch: | 13256 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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