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 25544U 26049.79608031 +.00000000 +00000-0 +18896-3 0 00003
2 25544 51.6323 165.7431 0010935 112.1599 248.0551 15.48691264 06
| Epoch (UTC): | 18 February 2026 19:06:21 |
| Eccentricity: | 0.0010935 |
| inclination: | 51.6323° |
| perigee height: | 413 km |
| apogee height: | 428 km |
| right ascension of ascending node: | 165.7431° |
| argument of perigee: | 112.1599° |
| revolutions per day: | 15.48691264 |
| mean anomaly at epoch: | 248.0551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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