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 41900U 26100.21650110 +.00000000 +00000-0 +13071-3 0 00007
2 41900 98.5475 92.6239 0023952 167.0194 193.1627 14.59709588 09
| Epoch (UTC): | 10 April 2026 05:11:45 |
| Eccentricity: | 0.0023952 |
| inclination: | 98.5475° |
| perigee height: | 677 km |
| apogee height: | 711 km |
| right ascension of ascending node: | 92.6239° |
| argument of perigee: | 167.0194° |
| revolutions per day: | 14.59709588 |
| mean anomaly at epoch: | 193.1627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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