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 35499U 26103.95673447 +.00000000 +00000-0 +24985-3 0 00001
2 35499 82.4859 119.5992 0014560 279.6084 80.3350 12.43007688 04
| Epoch (UTC): | 13 April 2026 22:57:41 |
| Eccentricity: | 0.0014560 |
| inclination: | 82.4859° |
| perigee height: | 1482 km |
| apogee height: | 1505 km |
| right ascension of ascending node: | 119.5992° |
| argument of perigee: | 279.6084° |
| revolutions per day: | 12.43007688 |
| mean anomaly at epoch: | 80.3350° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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