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 62176U 26144.93790883 +.00000000 +00000-0 +34551-3 0 00000
2 62176 70.0019 332.3105 0002325 269.7489 90.3403 14.98338470 01
| Epoch (UTC): | 24 May 2026 22:30:35 |
| Eccentricity: | 0.0002325 |
| inclination: | 70.0019° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 332.3105° |
| argument of perigee: | 269.7489° |
| revolutions per day: | 14.98338470 |
| mean anomaly at epoch: | 90.3403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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