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 60727U 26145.26790111 +.00000000 +00000-0 +23465-4 0 00004
2 60727 53.1593 98.6726 0001016 84.2143 275.8991 15.69717342 04
| Epoch (UTC): | 25 May 2026 06:25:46 |
| Eccentricity: | 0.0001016 |
| inclination: | 53.1593° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 98.6726° |
| argument of perigee: | 84.2143° |
| revolutions per day: | 15.69717342 |
| mean anomaly at epoch: | 275.8991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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