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 49217U 26145.33092139 +.00000000 +00000-0 +29885-3 0 00009
2 49217 87.9177 278.9950 0002130 109.3538 250.7826 13.20771931 03
| Epoch (UTC): | 25 May 2026 07:56:31 |
| Eccentricity: | 0.0002130 |
| inclination: | 87.9177° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9950° |
| argument of perigee: | 109.3538° |
| revolutions per day: | 13.20771931 |
| mean anomaly at epoch: | 250.7826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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