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 49134U 26145.22505655 +.00000000 +00000-0 +14836-4 0 00008
2 49134 69.9992 101.4865 0003689 258.8003 101.2741 14.98330861 03
| Epoch (UTC): | 25 May 2026 05:24:04 |
| Eccentricity: | 0.0003689 |
| inclination: | 69.9992° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 101.4865° |
| argument of perigee: | 258.8003° |
| revolutions per day: | 14.98330861 |
| mean anomaly at epoch: | 101.2741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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