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 55278U 26145.57056588 +.00000000 +00000-0 +67975-4 0 00000
2 55278 69.9992 210.5398 0003804 268.3541 91.7183 14.98325731 07
| Epoch (UTC): | 25 May 2026 13:41:36 |
| Eccentricity: | 0.0003804 |
| inclination: | 69.9992° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 210.5398° |
| argument of perigee: | 268.3541° |
| revolutions per day: | 14.98325731 |
| mean anomaly at epoch: | 91.7183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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