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 29507U 06046C 25201.58167227 .00003431 00000-0 18969-3 0 9994
2 29507 97.5939 242.1093 0034987 352.8331 7.2396 15.14061478 24891
| Epoch (UTC): | 20 July 2025 13:57:36 |
| Eccentricity: | 0.0034987 |
| inclination: | 97.5939° |
| perigee height: | 499 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 242.1093° |
| argument of perigee: | 352.8331° |
| revolutions per day: | 15.14061478 |
| mean anomaly at epoch: | 7.2396° |
| orbit number at epoch: | 2489 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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