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 56489U 26144.80768999 +.00000000 +00000-0 +14319-4 0 00000
2 56489 69.9992 272.5551 0003253 269.1086 90.9701 14.98332129 08
| Epoch (UTC): | 24 May 2026 19:23:04 |
| Eccentricity: | 0.0003253 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 272.5551° |
| argument of perigee: | 269.1086° |
| revolutions per day: | 14.98332129 |
| mean anomaly at epoch: | 90.9701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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