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 26104.03722369 +.00000000 +00000-0 +24024-3 0 00003
2 35499 82.4859 119.5490 0014558 279.4236 80.5198 12.43007687 02
| Epoch (UTC): | 14 April 2026 00:53:36 |
| Eccentricity: | 0.0014558 |
| inclination: | 82.4859° |
| perigee height: | 1482 km |
| apogee height: | 1505 km |
| right ascension of ascending node: | 119.5490° |
| argument of perigee: | 279.4236° |
| revolutions per day: | 12.43007687 |
| mean anomaly at epoch: | 80.5198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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