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 41914U 26145.49734594 +.00000000 +00000-0 +30131-3 0 00006
2 41914 97.1955 152.9120 0003853 242.2317 117.8539 15.40951389 06
| Epoch (UTC): | 25 May 2026 11:56:10 |
| Eccentricity: | 0.0003853 |
| inclination: | 97.1955° |
| perigee height: | 441 km |
| apogee height: | 446 km |
| right ascension of ascending node: | 152.9120° |
| argument of perigee: | 242.2317° |
| revolutions per day: | 15.40951389 |
| mean anomaly at epoch: | 117.8539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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