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 49061U 26088.07871463 +.00000000 +00000-0 +90097-4 0 00002
2 49061 89.0492 219.6015 0213636 51.4420 310.5715 14.48592414 09
| Epoch (UTC): | 29 March 2026 01:53:20 |
| Eccentricity: | 0.0213636 |
| inclination: | 89.0492° |
| perigee height: | 578 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 219.6015° |
| argument of perigee: | 51.4420° |
| revolutions per day: | 14.48592414 |
| mean anomaly at epoch: | 310.5715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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