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 25183.69207012 .07669060 80586-5 17140-3 0 9995
2 29252 64.4742 276.9705 0017693 300.1504 154.0455 16.44812741 50045
| Epoch (UTC): | 02 July 2025 16:36:34 |
| Eccentricity: | 0.0017693 |
| inclination: | 64.4742° |
| perigee height: | 141 km |
| apogee height: | 164 km |
| right ascension of ascending node: | 276.9705° |
| argument of perigee: | 300.1504° |
| revolutions per day: | 16.44812741 |
| mean anomaly at epoch: | 154.0455° |
| orbit number at epoch: | 5004 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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