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 data is extracted from the following two-line orbital elements,
1 35933U 09051C 25173.13999358 .00000614 00000-0 13595-3 0 9990
2 35933 98.4225 69.9418 0004028 267.6238 92.4501 14.60773894836603
| Epoch (UTC): | 22 June 2025 03:21:35 |
| Eccentricity: | 0.0004028 |
| inclination: | 98.4225° |
| perigee height: | 688 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 69.9418° |
| argument of perigee: | 267.6238° |
| revolutions per day: | 14.60773894 |
| mean anomaly at epoch: | 92.4501° |
| orbit number at epoch: | 83660 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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