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 55419U 26145.39577661 +.00000000 +00000-0 -29540-4 0 00004
2 55419 69.9993 250.9833 0003952 267.9163 92.1544 14.98332499 01
| Epoch (UTC): | 25 May 2026 09:29:55 |
| Eccentricity: | 0.0003952 |
| inclination: | 69.9993° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 250.9833° |
| argument of perigee: | 267.9163° |
| revolutions per day: | 14.98332499 |
| mean anomaly at epoch: | 92.1544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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