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 59721U 26145.26565753 +.00000000 +00000-0 +39431-4 0 00008
2 59721 53.1607 144.4076 0001120 81.6909 278.4219 15.30194683 04
| Epoch (UTC): | 25 May 2026 06:22:32 |
| Eccentricity: | 0.0001120 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 144.4076° |
| argument of perigee: | 81.6909° |
| revolutions per day: | 15.30194683 |
| mean anomaly at epoch: | 278.4219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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