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 is defined by the following mean orbital elements,
1 31304U 07015A 24232.50177551 .22339555 29440-5 37657-3 0 9997
2 31304 97.8504 218.1567 0008943 252.2283 207.7707 16.47607881953155
| Epoch (UTC): | 19 August 2024 12:02:33 |
| Eccentricity: | 0.0008943 |
| inclination: | 97.8504° |
| perigee height: | 140 km |
| apogee height: | 151 km |
| right ascension of ascending node: | 218.1567° |
| argument of perigee: | 252.2283° |
| revolutions per day: | 16.47607881 |
| mean anomaly at epoch: | 207.7707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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