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 55416U 26145.39995127 +.00000000 +00000-0 +29607-4 0 00005
2 55416 69.9995 250.9974 0003285 271.1077 88.9706 14.98332279 05
| Epoch (UTC): | 25 May 2026 09:35:55 |
| Eccentricity: | 0.0003285 |
| inclination: | 69.9995° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 250.9974° |
| argument of perigee: | 271.1077° |
| revolutions per day: | 14.98332279 |
| mean anomaly at epoch: | 88.9706° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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