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 41634U 26076.16549247 +.00000000 +00000-0 +91778-4 0 00006
2 41634 75.0012 93.1344 0008660 259.5858 100.4355 14.93247721 09
| Epoch (UTC): | 17 March 2026 03:58:18 |
| Eccentricity: | 0.0008660 |
| inclination: | 75.0012° |
| perigee height: | 582 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 93.1344° |
| argument of perigee: | 259.5858° |
| revolutions per day: | 14.93247721 |
| mean anomaly at epoch: | 100.4355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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