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 62121U 26145.46265096 +.00000000 +00000-0 +59485-3 0 00005
2 62121 42.9989 62.3323 0000736 236.4632 123.6150 15.27622964 08
| Epoch (UTC): | 25 May 2026 11:06:13 |
| Eccentricity: | 0.0000736 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 62.3323° |
| argument of perigee: | 236.4632° |
| revolutions per day: | 15.27622964 |
| mean anomaly at epoch: | 123.6150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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