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 23154.55067928 .00002139 00000-0 15817-3 0 9999
2 29228 69.9357 313.3863 0007445 250.1639 109.8721 15.04811102935195
| Epoch (UTC): | 03 June 2023 13:12:58 |
| Eccentricity: | 0.0007445 |
| inclination: | 69.9357° |
| perigee height: | 547 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 313.3863° |
| argument of perigee: | 250.1639° |
| revolutions per day: | 15.04811102 |
| mean anomaly at epoch: | 109.8721° |
| orbit number at epoch: | 93519 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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