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 26045.98021447 +.00000000 +00000-0 +20471-3 0 00005
2 35933 98.4052 311.6038 0004036 243.3333 116.7454 14.61475788 08
| Epoch (UTC): | 14 February 2026 23:31:30 |
| Eccentricity: | 0.0004036 |
| inclination: | 98.4052° |
| perigee height: | 686 km |
| apogee height: | 691 km |
| right ascension of ascending node: | 311.6038° |
| argument of perigee: | 243.3333° |
| revolutions per day: | 14.61475788 |
| mean anomaly at epoch: | 116.7454° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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