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 65978U 26145.49338227 +.00000000 +00000-0 -62396-2 0 00003
2 65978 81.3006 232.5254 0002377 273.4172 86.6713 13.85413327 01
| Epoch (UTC): | 25 May 2026 11:50:28 |
| Eccentricity: | 0.0002377 |
| inclination: | 81.3006° |
| perigee height: | 943 km |
| apogee height: | 946 km |
| right ascension of ascending node: | 232.5254° |
| argument of perigee: | 273.4172° |
| revolutions per day: | 13.85413327 |
| mean anomaly at epoch: | 86.6713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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