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 49415U 26145.54396699 +.00000000 +00000-0 +66518-4 0 00005
2 49415 53.2125 234.1099 0001163 91.8645 268.2480 15.08837160 04
| Epoch (UTC): | 25 May 2026 13:03:18 |
| Eccentricity: | 0.0001163 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 234.1099° |
| argument of perigee: | 91.8645° |
| revolutions per day: | 15.08837160 |
| mean anomaly at epoch: | 268.2480° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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