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 35200U 99025DPG 24351.53023049 .00000506 00000-0 67625-3 0 9996
2 35200 98.8546 6.5880 0352582 250.2658 268.4586 13.41648784833900
| Epoch (UTC): | 16 December 2024 12:43:31 |
| Eccentricity: | 0.0352582 |
| inclination: | 98.8546° |
| perigee height: | 839 km |
| apogee height: | 1367 km |
| right ascension of ascending node: | 6.5880° |
| argument of perigee: | 250.2658° |
| revolutions per day: | 13.41648784 |
| mean anomaly at epoch: | 268.4586° |
| orbit number at epoch: | 83390 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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