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 29228U 06021A 22334.68515576 .00001199 00000-0 94534-4 0 9998
2 29228 69.9363 65.2486 0004625 206.8059 153.2864 15.03680836907396
| Epoch (UTC): | 30 November 2022 16:26:37 |
| Eccentricity: | 0.0004625 |
| inclination: | 69.9363° |
| perigee height: | 552 km |
| apogee height: | 559 km |
| right ascension of ascending node: | 65.2486° |
| argument of perigee: | 206.8059° |
| revolutions per day: | 15.03680836 |
| mean anomaly at epoch: | 153.2864° |
| orbit number at epoch: | 90739 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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