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 56448U 26145.45923447 +.00000000 +00000-0 +33283-4 0 00009
2 56448 69.9988 310.9617 0002849 266.3756 93.7078 14.98331463 09
| Epoch (UTC): | 25 May 2026 11:01:17 |
| Eccentricity: | 0.0002849 |
| inclination: | 69.9988° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 310.9617° |
| argument of perigee: | 266.3756° |
| revolutions per day: | 14.98331463 |
| mean anomaly at epoch: | 93.7078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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