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 data is extracted from the following two-line orbital elements,
1 03029U 67111A 23088.62425473 -.00000094 00000-0 00000-0 0 9998
2 03029 0.1566 71.9233 0019227 20.2016 214.0719 1.00271573202847
| Epoch (UTC): | 29 March 2023 14:58:55 |
| Eccentricity: | 0.0019227 |
| inclination: | 0.1566° |
| perigee height: | 35705 km |
| apogee height: | 35867 km |
| right ascension of ascending node: | 71.9233° |
| argument of perigee: | 20.2016° |
| revolutions per day: | 1.00271573 |
| mean anomaly at epoch: | 214.0719° |
| orbit number at epoch: | 20284 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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