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 25398U 26145.41654762 +.00000000 +00000-0 +14973-4 0 00001
2 25398 99.0127 130.9271 0000327 299.8560 60.2585 14.23051914 07
| Epoch (UTC): | 25 May 2026 09:59:49 |
| Eccentricity: | 0.0000327 |
| inclination: | 99.0127° |
| perigee height: | 815 km |
| apogee height: | 815 km |
| right ascension of ascending node: | 130.9271° |
| argument of perigee: | 299.8560° |
| revolutions per day: | 14.23051914 |
| mean anomaly at epoch: | 60.2585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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