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 66701U 26145.14357172 +.00000000 +00000-0 +33757-3 0 00009
2 66701 97.4221 219.1437 0005960 86.1865 274.0051 15.19909021 04
| Epoch (UTC): | 25 May 2026 03:26:44 |
| Eccentricity: | 0.0005960 |
| inclination: | 97.4221° |
| perigee height: | 502 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 219.1437° |
| argument of perigee: | 86.1865° |
| revolutions per day: | 15.19909021 |
| mean anomaly at epoch: | 274.0051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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