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 35498U 26145.59703595 +.00000000 +00000-0 +25297-3 0 00001
2 35498 82.4860 106.3788 0005455 261.7440 98.3019 12.40870136 07
| Epoch (UTC): | 25 May 2026 14:19:43 |
| Eccentricity: | 0.0005455 |
| inclination: | 82.4860° |
| perigee height: | 1499 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 106.3788° |
| argument of perigee: | 261.7440° |
| revolutions per day: | 12.40870136 |
| mean anomaly at epoch: | 98.3019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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