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 66738U 26145.45935997 +.00000000 +00000-0 +22150-3 0 00005
2 66738 97.4203 219.5922 0002465 50.7689 309.3764 15.20369137 08
| Epoch (UTC): | 25 May 2026 11:01:28 |
| Eccentricity: | 0.0002465 |
| inclination: | 97.4203° |
| perigee height: | 503 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 219.5922° |
| argument of perigee: | 50.7689° |
| revolutions per day: | 15.20369137 |
| mean anomaly at epoch: | 309.3764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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