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 59212U 26145.35849192 +.00000000 +00000-0 +21993-4 0 00009
2 59212 53.1598 159.5139 0001185 88.1090 272.0047 15.30191112 02
| Epoch (UTC): | 25 May 2026 08:36:13 |
| Eccentricity: | 0.0001185 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 159.5139° |
| argument of perigee: | 88.1090° |
| revolutions per day: | 15.30191112 |
| mean anomaly at epoch: | 272.0047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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