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 60288U 26145.16423874 +.00000000 +00000-0 +47710-4 0 00003
2 60288 53.1612 56.8792 0001301 85.1784 274.9365 15.30195213 05
| Epoch (UTC): | 25 May 2026 03:56:30 |
| Eccentricity: | 0.0001301 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 56.8792° |
| argument of perigee: | 85.1784° |
| revolutions per day: | 15.30195213 |
| mean anomaly at epoch: | 274.9365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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