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 49115U 26145.56405500 +.00000000 +00000-0 +00000-0 0 00006
2 49115 0.4525 86.3105 0002244 319.8327 300.6088 1.00271389 02
| Epoch (UTC): | 25 May 2026 13:32:14 |
| Eccentricity: | 0.0002244 |
| inclination: | 0.4525° |
| perigee height: | 35777 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 86.3105° |
| argument of perigee: | 319.8327° |
| revolutions per day: | 1.00271389 |
| mean anomaly at epoch: | 300.6088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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