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 29710U 07001B 24045.26546296 .15373921 28539-5 20784-3 0 9999
2 29710 97.8588 219.0513 0007525 281.0118 81.3478 16.49055820930314
| Epoch (UTC): | 14 February 2024 06:22:16 |
| Eccentricity: | 0.0007525 |
| inclination: | 97.8588° |
| perigee height: | 137 km |
| apogee height: | 147 km |
| right ascension of ascending node: | 219.0513° |
| argument of perigee: | 281.0118° |
| revolutions per day: | 16.49055820 |
| mean anomaly at epoch: | 81.3478° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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