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 61072U 26145.63722889 +.00000000 +00000-0 +26870-3 0 00008
2 61072 64.0746 116.3118 0052002 308.0587 51.5841 15.10878553 03
| Epoch (UTC): | 25 May 2026 15:17:36 |
| Eccentricity: | 0.0052002 |
| inclination: | 64.0746° |
| perigee height: | 498 km |
| apogee height: | 569 km |
| right ascension of ascending node: | 116.3118° |
| argument of perigee: | 308.0587° |
| revolutions per day: | 15.10878553 |
| mean anomaly at epoch: | 51.5841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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