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 35933U 26106.70510473 +.00000000 +00000-0 +11495-3 0 00001
2 35933 98.4000 13.2810 0006498 63.9237 296.2631 14.61617266 07
| Epoch (UTC): | 16 April 2026 16:55:21 |
| Eccentricity: | 0.0006498 |
| inclination: | 98.4000° |
| perigee height: | 683 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 13.2810° |
| argument of perigee: | 63.9237° |
| revolutions per day: | 14.61617266 |
| mean anomaly at epoch: | 296.2631° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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