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 61708U 26145.61156185 +.00000000 +00000-0 +91441-4 0 00009
2 61708 53.1611 104.0491 0001173 94.0685 266.0450 15.30210774 07
| Epoch (UTC): | 25 May 2026 14:40:38 |
| Eccentricity: | 0.0001173 |
| inclination: | 53.1611° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 104.0491° |
| argument of perigee: | 94.0685° |
| revolutions per day: | 15.30210774 |
| mean anomaly at epoch: | 266.0450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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