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 60270U 26145.16855784 +.00000000 +00000-0 +41795-4 0 00000
2 60270 53.1611 57.5055 0001186 75.2701 284.8431 15.30194987 06
| Epoch (UTC): | 25 May 2026 04:02:43 |
| Eccentricity: | 0.0001186 |
| inclination: | 53.1611° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 57.5055° |
| argument of perigee: | 75.2701° |
| revolutions per day: | 15.30194987 |
| mean anomaly at epoch: | 284.8431° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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