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 55754U 26145.47273705 +.00000000 +00000-0 +52728-5 0 00001
2 55754 70.0002 50.7769 0002746 270.0186 90.0659 14.98329412 06
| Epoch (UTC): | 25 May 2026 11:20:44 |
| Eccentricity: | 0.0002746 |
| inclination: | 70.0002° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 50.7769° |
| argument of perigee: | 270.0186° |
| revolutions per day: | 14.98329412 |
| mean anomaly at epoch: | 90.0659° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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