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 49495U 26145.57043926 +.00000000 +00000-0 +28039-4 0 00004
2 49495 98.4097 153.9889 0003911 66.9309 293.2292 14.42213565 02
| Epoch (UTC): | 25 May 2026 13:41:25 |
| Eccentricity: | 0.0003911 |
| inclination: | 98.4097° |
| perigee height: | 748 km |
| apogee height: | 754 km |
| right ascension of ascending node: | 153.9889° |
| argument of perigee: | 66.9309° |
| revolutions per day: | 14.42213565 |
| mean anomaly at epoch: | 293.2292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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