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 49421U 26145.57246581 +.00000000 +00000-0 +32472-4 0 00001
2 49421 53.2144 243.7886 0000843 83.1554 276.9534 15.08836165 09
| Epoch (UTC): | 25 May 2026 13:44:21 |
| Eccentricity: | 0.0000843 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 243.7886° |
| argument of perigee: | 83.1554° |
| revolutions per day: | 15.08836165 |
| mean anomaly at epoch: | 276.9534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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