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 62995U 26145.17715508 +.00000000 +00000-0 +41810-3 0 00003
2 62995 43.0030 71.3207 0001546 275.0170 85.0505 15.27588933 05
| Epoch (UTC): | 25 May 2026 04:15:06 |
| Eccentricity: | 0.0001546 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 71.3207° |
| argument of perigee: | 275.0170° |
| revolutions per day: | 15.27588933 |
| mean anomaly at epoch: | 85.0505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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