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 56813U 26145.45736190 +.00000000 +00000-0 +43423-5 0 00000
2 56813 69.9985 150.7213 0003570 266.0217 94.0534 14.98331850 06
| Epoch (UTC): | 25 May 2026 10:58:36 |
| Eccentricity: | 0.0003570 |
| inclination: | 69.9985° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 150.7213° |
| argument of perigee: | 266.0217° |
| revolutions per day: | 14.98331850 |
| mean anomaly at epoch: | 94.0534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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