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 41335U 26153.91007124 +.00000000 +00000-0 +71997-4 0 00007
2 41335 98.6252 221.4981 0001302 106.0003 254.1321 14.26735741 01
| Epoch (UTC): | 02 June 2026 21:50:30 |
| Eccentricity: | 0.0001302 |
| inclination: | 98.6252° |
| perigee height: | 802 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 221.4981° |
| argument of perigee: | 106.0003° |
| revolutions per day: | 14.26735741 |
| mean anomaly at epoch: | 254.1321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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