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 49729U 26145.46483425 +.00000000 +00000-0 +54926-4 0 00008
2 49729 53.2128 174.3494 0001056 65.1514 294.9588 15.08841281 03
| Epoch (UTC): | 25 May 2026 11:09:21 |
| Eccentricity: | 0.0001056 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 174.3494° |
| argument of perigee: | 65.1514° |
| revolutions per day: | 15.08841281 |
| mean anomaly at epoch: | 294.9588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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