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 62517U 26145.50221118 +.00000000 +00000-0 +99973-3 0 00002
2 62517 42.9996 327.3267 0002974 277.7797 82.2732 15.70879089 08
| Epoch (UTC): | 25 May 2026 12:03:11 |
| Eccentricity: | 0.0002974 |
| inclination: | 42.9996° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 327.3267° |
| argument of perigee: | 277.7797° |
| revolutions per day: | 15.70879089 |
| mean anomaly at epoch: | 82.2732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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