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 62173U 26145.49047663 +.00000000 +00000-0 +39880-3 0 00000
2 62173 70.0014 320.6220 0002521 274.1209 85.9662 14.98333239 04
| Epoch (UTC): | 25 May 2026 11:46:17 |
| Eccentricity: | 0.0002521 |
| inclination: | 70.0014° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 320.6220° |
| argument of perigee: | 274.1209° |
| revolutions per day: | 14.98333239 |
| mean anomaly at epoch: | 85.9662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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