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 49425U 26144.98464715 +.00000000 +00000-0 +91313-4 0 00009
2 49425 53.2147 246.6307 0001277 90.7686 269.3453 15.08834116 08
| Epoch (UTC): | 24 May 2026 23:37:53 |
| Eccentricity: | 0.0001277 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 246.6307° |
| argument of perigee: | 90.7686° |
| revolutions per day: | 15.08834116 |
| mean anomaly at epoch: | 269.3453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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