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 26074.80305299 +.00000000 +00000-0 +19683-3 0 00001
2 35933 98.4025 340.8821 0005714 145.5133 214.6439 14.61547690 00
| Epoch (UTC): | 15 March 2026 19:16:23 |
| Eccentricity: | 0.0005714 |
| inclination: | 98.4025° |
| perigee height: | 684 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 340.8821° |
| argument of perigee: | 145.5133° |
| revolutions per day: | 14.61547690 |
| mean anomaly at epoch: | 214.6439° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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