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 35865U 26113.65834759 +.00000000 +00000-0 +46469-4 0 00003
2 35865 98.7345 76.5382 0003318 100.5128 259.6424 14.23143778 00
| Epoch (UTC): | 23 April 2026 15:48:01 |
| Eccentricity: | 0.0003318 |
| inclination: | 98.7345° |
| perigee height: | 812 km |
| apogee height: | 817 km |
| right ascension of ascending node: | 76.5382° |
| argument of perigee: | 100.5128° |
| revolutions per day: | 14.23143778 |
| mean anomaly at epoch: | 259.6424° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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