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 31135U 07013A 24039.00000000 .02708747 -37185-4 64323-3 0 9997
2 31135 2.4637 60.5051 0002597 58.1662 329.6832 16.28281628937887
| Epoch (UTC): | 08 February 2024 00:00:00 |
| Eccentricity: | 0.0002597 |
| inclination: | 2.4637° |
| perigee height: | 195 km |
| apogee height: | 199 km |
| right ascension of ascending node: | 60.5051° |
| argument of perigee: | 58.1662° |
| revolutions per day: | 16.28281628 |
| mean anomaly at epoch: | 329.6832° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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