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 61715U 26145.27445528 +.00000000 +00000-0 +14704-4 0 00008
2 61715 53.1617 105.4962 0001323 89.8577 270.2575 15.30188586 08
| Epoch (UTC): | 25 May 2026 06:35:12 |
| Eccentricity: | 0.0001323 |
| inclination: | 53.1617° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 105.4962° |
| argument of perigee: | 89.8577° |
| revolutions per day: | 15.30188586 |
| mean anomaly at epoch: | 270.2575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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