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 35870U 09049F 21343.64242906 .02501710 22463-5 32104-3 0 9992
2 35870 96.9213 23.3078 0006438 229.6871 257.1968 16.35882066689336
| Epoch (UTC): | 09 December 2021 15:25:05 |
| Eccentricity: | 0.0006438 |
| inclination: | 96.9213° |
| perigee height: | 172 km |
| apogee height: | 181 km |
| right ascension of ascending node: | 23.3078° |
| argument of perigee: | 229.6871° |
| revolutions per day: | 16.35882066 |
| mean anomaly at epoch: | 257.1968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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