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 61521U 26145.22509802 +.00000000 +00000-0 +23726-4 0 00008
2 61521 53.1586 146.7047 0001122 85.2595 274.8534 15.30195177 06
| Epoch (UTC): | 25 May 2026 05:24:08 |
| Eccentricity: | 0.0001122 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 146.7047° |
| argument of perigee: | 85.2595° |
| revolutions per day: | 15.30195177 |
| mean anomaly at epoch: | 274.8534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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