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 66772U 26145.45585444 +.00000000 +00000-0 +27214-3 0 00007
2 66772 97.4239 219.8257 0000411 59.2460 300.8816 15.21105766 00
| Epoch (UTC): | 25 May 2026 10:56:25 |
| Eccentricity: | 0.0000411 |
| inclination: | 97.4239° |
| perigee height: | 502 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 219.8257° |
| argument of perigee: | 59.2460° |
| revolutions per day: | 15.21105766 |
| mean anomaly at epoch: | 300.8816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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