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 61530U 26145.37486713 +.00000000 +00000-0 +32980-4 0 00001
2 61530 53.1600 146.2332 0001142 96.3990 263.7141 15.31694005 05
| Epoch (UTC): | 25 May 2026 08:59:48 |
| Eccentricity: | 0.0001142 |
| inclination: | 53.1600° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 146.2332° |
| argument of perigee: | 96.3990° |
| revolutions per day: | 15.31694005 |
| mean anomaly at epoch: | 263.7141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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