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 60295U 26145.13367649 +.00000000 +00000-0 +24380-4 0 00003
2 60295 53.1610 57.4001 0001158 95.1312 264.9822 15.31700302 08
| Epoch (UTC): | 25 May 2026 03:12:29 |
| Eccentricity: | 0.0001158 |
| inclination: | 53.1610° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 57.4001° |
| argument of perigee: | 95.1312° |
| revolutions per day: | 15.31700302 |
| mean anomaly at epoch: | 264.9822° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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