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 61709U 26145.26812132 +.00000000 +00000-0 +18932-4 0 00006
2 61709 53.1606 105.4567 0001021 99.5253 260.5863 15.30193691 09
| Epoch (UTC): | 25 May 2026 06:26:05 |
| Eccentricity: | 0.0001021 |
| inclination: | 53.1606° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 105.4567° |
| argument of perigee: | 99.5253° |
| revolutions per day: | 15.30193691 |
| mean anomaly at epoch: | 260.5863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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