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 61512U 26145.37100368 +.00000000 +00000-0 +21173-4 0 00002
2 61512 53.1589 133.4179 0001207 76.1021 284.0114 15.30195700 04
| Epoch (UTC): | 25 May 2026 08:54:14 |
| Eccentricity: | 0.0001207 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 133.4179° |
| argument of perigee: | 76.1021° |
| revolutions per day: | 15.30195700 |
| mean anomaly at epoch: | 284.0114° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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