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 60725U 26145.15038368 +.00000000 +00000-0 +30670-4 0 00005
2 60725 53.1587 99.3672 0000969 79.8875 280.2252 15.69692361 04
| Epoch (UTC): | 25 May 2026 03:36:33 |
| Eccentricity: | 0.0000969 |
| inclination: | 53.1587° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 99.3672° |
| argument of perigee: | 79.8875° |
| revolutions per day: | 15.69692361 |
| mean anomaly at epoch: | 280.2252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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