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 26161.50657164 +.00000000 +00000-0 +34249-6 0 00001
2 35499 82.4905 83.7485 0016103 148.7876 211.4163 12.43009238 07
| Epoch (UTC): | 10 June 2026 12:09:27 |
| Eccentricity: | 0.0016103 |
| inclination: | 82.4905° |
| perigee height: | 1481 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 83.7485° |
| argument of perigee: | 148.7876° |
| revolutions per day: | 12.43009238 |
| mean anomaly at epoch: | 211.4163° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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