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 is defined by the following mean orbital elements,
1 25504U 26088.02986464 +.00000000 +00000-0 +70650-4 0 00004
2 25504 24.9946 206.4784 0016802 356.9692 163.8858 14.45492630 07
| Epoch (UTC): | 29 March 2026 00:43:00 |
| Eccentricity: | 0.0016802 |
| inclination: | 24.9946° |
| perigee height: | 728 km |
| apogee height: | 752 km |
| right ascension of ascending node: | 206.4784° |
| argument of perigee: | 356.9692° |
| revolutions per day: | 14.45492630 |
| mean anomaly at epoch: | 163.8858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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