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 61212U 26145.33652183 +.00000000 +00000-0 +31348-4 0 00007
2 61212 53.1586 158.6626 0001162 73.2334 286.8811 15.69711927 00
| Epoch (UTC): | 25 May 2026 08:04:35 |
| Eccentricity: | 0.0001162 |
| inclination: | 53.1586° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 158.6626° |
| argument of perigee: | 73.2334° |
| revolutions per day: | 15.69711927 |
| mean anomaly at epoch: | 286.8811° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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