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 59221U 26145.35705505 +.00000000 +00000-0 +27514-4 0 00003
2 59221 53.1601 158.0944 0001254 87.3765 272.7381 15.34385308 06
| Epoch (UTC): | 25 May 2026 08:34:09 |
| Eccentricity: | 0.0001254 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 158.0944° |
| argument of perigee: | 87.3765° |
| revolutions per day: | 15.34385308 |
| mean anomaly at epoch: | 272.7381° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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