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 25113U 26088.05410586 +.00000000 +00000-0 +45850-3 0 00003
2 25113 45.0145 82.0286 0005657 242.3794 117.6484 14.46764230 01
| Epoch (UTC): | 29 March 2026 01:17:54 |
| Eccentricity: | 0.0005657 |
| inclination: | 45.0145° |
| perigee height: | 732 km |
| apogee height: | 740 km |
| right ascension of ascending node: | 82.0286° |
| argument of perigee: | 242.3794° |
| revolutions per day: | 14.46764230 |
| mean anomaly at epoch: | 117.6484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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