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 35495U 26159.85245975 +.00000000 +00000-0 +10471-2 0 00002
2 35495 49.6182 25.8770 4886246 104.8728 312.4300 5.80510624 09
| Epoch (UTC): | 08 June 2026 20:27:32 |
| Eccentricity: | 0.4886246 |
| inclination: | 49.6182° |
| perigee height: | 309 km |
| apogee height: | 13090 km |
| right ascension of ascending node: | 25.8770° |
| argument of perigee: | 104.8728° |
| revolutions per day: | 5.80510624 |
| mean anomaly at epoch: | 312.4300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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