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 62414U 26145.18983310 +.00000000 +00000-0 +13098-2 0 00004
2 62414 43.0043 66.3986 0002616 256.8087 103.2489 15.70892990 09
| Epoch (UTC): | 25 May 2026 04:33:21 |
| Eccentricity: | 0.0002616 |
| inclination: | 43.0043° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 66.3986° |
| argument of perigee: | 256.8087° |
| revolutions per day: | 15.70892990 |
| mean anomaly at epoch: | 103.2489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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