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 62914U 26145.33560178 +.00000000 +00000-0 +15703-2 0 00004
2 62914 43.0016 245.9249 0002310 258.6806 101.3802 15.70945876 01
| Epoch (UTC): | 25 May 2026 08:03:15 |
| Eccentricity: | 0.0002310 |
| inclination: | 43.0016° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 245.9249° |
| argument of perigee: | 258.6806° |
| revolutions per day: | 15.70945876 |
| mean anomaly at epoch: | 101.3802° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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