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 59211U 26145.40531206 +.00000000 +00000-0 +62589-4 0 00004
2 59211 53.1602 146.3236 0001306 90.4556 269.6594 15.30193776 04
| Epoch (UTC): | 25 May 2026 09:43:38 |
| Eccentricity: | 0.0001306 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 146.3236° |
| argument of perigee: | 90.4556° |
| revolutions per day: | 15.30193776 |
| mean anomaly at epoch: | 269.6594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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