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 35935U 26032.22851293 +.00000000 +00000-0 +25069-3 0 00008
2 35935 98.4151 296.9628 0006545 307.7519 52.3087 14.60180535 07
| Epoch (UTC): | 01 February 2026 05:29:03 |
| Eccentricity: | 0.0006545 |
| inclination: | 98.4151° |
| perigee height: | 688 km |
| apogee height: | 697 km |
| right ascension of ascending node: | 296.9628° |
| argument of perigee: | 307.7519° |
| revolutions per day: | 14.60180535 |
| mean anomaly at epoch: | 52.3087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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