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 60428U 26145.22376065 +.00000000 +00000-0 +50463-4 0 00004
2 60428 53.1600 221.8690 0001147 77.2433 282.8696 15.30197704 02
| Epoch (UTC): | 25 May 2026 05:22:12 |
| Eccentricity: | 0.0001147 |
| inclination: | 53.1600° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 221.8690° |
| argument of perigee: | 77.2433° |
| revolutions per day: | 15.30197704 |
| mean anomaly at epoch: | 282.8696° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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