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 62670U 26145.19595612 +.00000000 +00000-0 +38701-3 0 00002
2 62670 97.3924 226.4878 0005678 69.5620 290.6229 15.28746814 04
| Epoch (UTC): | 25 May 2026 04:42:10 |
| Eccentricity: | 0.0005678 |
| inclination: | 97.3924° |
| perigee height: | 476 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 226.4878° |
| argument of perigee: | 69.5620° |
| revolutions per day: | 15.28746814 |
| mean anomaly at epoch: | 290.6229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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