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 60931U 26145.21524848 +.00000000 +00000-0 +29452-4 0 00000
2 60931 53.1568 323.8548 0000953 93.4343 266.6784 15.69715359 05
| Epoch (UTC): | 25 May 2026 05:09:57 |
| Eccentricity: | 0.0000953 |
| inclination: | 53.1568° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 323.8548° |
| argument of perigee: | 93.4343° |
| revolutions per day: | 15.69715359 |
| mean anomaly at epoch: | 266.6784° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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