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 35008U 09029A 21113.17436894 .99999999 84750-5 53592-3 0 9994
2 35008 62.9229 132.8490 0188760 266.4628 205.8679 16.29926844 98745
| Epoch (UTC): | 23 April 2021 04:11:05 |
| Eccentricity: | 0.0188760 |
| inclination: | 62.9229° |
| perigee height: | 69 km |
| apogee height: | 317 km |
| right ascension of ascending node: | 132.8490° |
| argument of perigee: | 266.4628° |
| revolutions per day: | 16.29926844 |
| mean anomaly at epoch: | 205.8679° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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