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 58702U 24004C 24277.16814036 .00015602 00000-0 78561-3 0 9997
2 58702 97.4606 96.4132 0008234 45.6940 314.4967 15.17251409 41123
| Epoch (UTC): | 03 October 2024 04:02:07 |
| Eccentricity: | 0.0008234 |
| inclination: | 97.4606° |
| perigee height: | 508 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 96.4132° |
| argument of perigee: | 45.6940° |
| revolutions per day: | 15.17251409 |
| mean anomaly at epoch: | 314.4967° |
| orbit number at epoch: | 4112 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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