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 35496U 26145.47585941 +.00000000 +00000-0 +00000-0 0 00001
2 35496 5.1723 48.8047 0002831 10.2222 244.3278 1.00270639 09
| Epoch (UTC): | 25 May 2026 11:25:14 |
| Eccentricity: | 0.0002831 |
| inclination: | 5.1723° |
| perigee height: | 35775 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 48.8047° |
| argument of perigee: | 10.2222° |
| revolutions per day: | 1.00270639 |
| mean anomaly at epoch: | 244.3278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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