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 65521U 26145.45572869 +.00000000 +00000-0 +17325-2 0 00006
2 65521 97.4533 215.1204 0001066 135.3457 224.7856 15.05723058 08
| Epoch (UTC): | 25 May 2026 10:56:14 |
| Eccentricity: | 0.0001066 |
| inclination: | 97.4533° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 215.1204° |
| argument of perigee: | 135.3457° |
| revolutions per day: | 15.05723058 |
| mean anomaly at epoch: | 224.7856° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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