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 26150.43620220 +.00000000 +00000-0 +69864-4 0 00009
2 25504 24.9937 181.6299 0016509 296.0994 195.8407 14.45518079 06
| Epoch (UTC): | 30 May 2026 10:28:07 |
| Eccentricity: | 0.0016509 |
| inclination: | 24.9937° |
| perigee height: | 729 km |
| apogee height: | 752 km |
| right ascension of ascending node: | 181.6299° |
| argument of perigee: | 296.0994° |
| revolutions per day: | 14.45518079 |
| mean anomaly at epoch: | 195.8407° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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