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 61522U 26145.41729245 +.00000000 +00000-0 +19737-3 0 00001
2 61522 53.1578 145.7708 0001428 65.6966 294.4184 15.30339613 08
| Epoch (UTC): | 25 May 2026 10:00:54 |
| Eccentricity: | 0.0001428 |
| inclination: | 53.1578° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 145.7708° |
| argument of perigee: | 65.6966° |
| revolutions per day: | 15.30339613 |
| mean anomaly at epoch: | 294.4184° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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