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 66727U 26145.10329230 +.00000000 +00000-0 +27010-3 0 00002
2 66727 97.4240 219.0937 0005643 95.3213 264.8666 15.19533517 06
| Epoch (UTC): | 25 May 2026 02:28:44 |
| Eccentricity: | 0.0005643 |
| inclination: | 97.4240° |
| perigee height: | 503 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 219.0937° |
| argument of perigee: | 95.3213° |
| revolutions per day: | 15.19533517 |
| mean anomaly at epoch: | 264.8666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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