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 41774U 26145.12575263 +.00000000 +00000-0 +36843-3 0 00002
2 41774 96.9040 176.8746 0002658 82.0747 278.0808 15.51448926 09
| Epoch (UTC): | 25 May 2026 03:01:05 |
| Eccentricity: | 0.0002658 |
| inclination: | 96.9040° |
| perigee height: | 411 km |
| apogee height: | 414 km |
| right ascension of ascending node: | 176.8746° |
| argument of perigee: | 82.0747° |
| revolutions per day: | 15.51448926 |
| mean anomaly at epoch: | 278.0808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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