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 62175U 26145.48033676 +.00000000 +00000-0 +11325-3 0 00004
2 62175 70.0015 330.9954 0002613 266.7314 93.3547 14.98334167 07
| Epoch (UTC): | 25 May 2026 11:31:41 |
| Eccentricity: | 0.0002613 |
| inclination: | 70.0015° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 330.9954° |
| argument of perigee: | 266.7314° |
| revolutions per day: | 14.98334167 |
| mean anomaly at epoch: | 93.3547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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