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 29252U 06029A 23152.28400059 .00009019 00000-0 34782-3 0 9994
2 29252 64.5211 1.6107 0027566 214.0874 145.8484 15.26525391932094
| Epoch (UTC): | 01 June 2023 06:48:57 |
| Eccentricity: | 0.0027566 |
| inclination: | 64.5211° |
| perigee height: | 467 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 1.6107° |
| argument of perigee: | 214.0874° |
| revolutions per day: | 15.26525391 |
| mean anomaly at epoch: | 145.8484° |
| orbit number at epoch: | 93209 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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