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 49414U 26145.55419591 +.00000000 +00000-0 -12945-2 0 00006
2 49414 53.2147 244.0615 0001406 65.7163 294.3975 15.08722068 05
| Epoch (UTC): | 25 May 2026 13:18:02 |
| Eccentricity: | 0.0001406 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 244.0615° |
| argument of perigee: | 65.7163° |
| revolutions per day: | 15.08722068 |
| mean anomaly at epoch: | 294.3975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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