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 55273U 26145.42452237 +.00000000 +00000-0 +92320-4 0 00002
2 55273 69.9992 210.8380 0003528 266.3112 93.7644 14.98332382 05
| Epoch (UTC): | 25 May 2026 10:11:18 |
| Eccentricity: | 0.0003528 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 210.8380° |
| argument of perigee: | 266.3112° |
| revolutions per day: | 14.98332382 |
| mean anomaly at epoch: | 93.7644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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