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 61728U 26145.27762182 +.00000000 +00000-0 -27026-4 0 00002
2 61728 53.1606 105.5148 0001214 81.9976 278.1163 15.30181616 09
| Epoch (UTC): | 25 May 2026 06:39:46 |
| Eccentricity: | 0.0001214 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 105.5148° |
| argument of perigee: | 81.9976° |
| revolutions per day: | 15.30181616 |
| mean anomaly at epoch: | 278.1163° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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