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 42562U 72058JV 24356.29258385 .00003124 00000-0 65179-3 0 9994
2 42562 98.8181 164.4511 0155293 228.8053 129.9665 14.53410027586184
| Epoch (UTC): | 21 December 2024 07:01:19 |
| Eccentricity: | 0.0155293 |
| inclination: | 98.8181° |
| perigee height: | 604 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 164.4511° |
| argument of perigee: | 228.8053° |
| revolutions per day: | 14.53410027 |
| mean anomaly at epoch: | 129.9665° |
| orbit number at epoch: | 58618 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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