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 49154U 26145.54199992 +.00000000 +00000-0 -24102-3 0 00005
2 49154 70.0003 81.7050 0003049 266.0215 94.0595 14.97535401 05
| Epoch (UTC): | 25 May 2026 13:00:28 |
| Eccentricity: | 0.0003049 |
| inclination: | 70.0003° |
| perigee height: | 572 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 81.7050° |
| argument of perigee: | 266.0215° |
| revolutions per day: | 14.97535401 |
| mean anomaly at epoch: | 94.0595° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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