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 26145.51347749 +.00000000 +00000-0 +44868-4 0 00001
2 25504 24.9942 211.9894 0016488 243.3017 139.4397 14.45515642 02
| Epoch (UTC): | 25 May 2026 12:19:24 |
| Eccentricity: | 0.0016488 |
| inclination: | 24.9942° |
| perigee height: | 729 km |
| apogee height: | 752 km |
| right ascension of ascending node: | 211.9894° |
| argument of perigee: | 243.3017° |
| revolutions per day: | 14.45515642 |
| mean anomaly at epoch: | 139.4397° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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