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 49001U 26145.51423955 +.00000000 +00000-0 +71936-4 0 00009
2 49001 87.9102 233.2812 0001941 96.4056 263.7296 13.16592871 07
| Epoch (UTC): | 25 May 2026 12:20:30 |
| Eccentricity: | 0.0001941 |
| inclination: | 87.9102° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2812° |
| argument of perigee: | 96.4056° |
| revolutions per day: | 13.16592871 |
| mean anomaly at epoch: | 263.7296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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