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 26047.21491617 +.00000000 +00000-0 +19660-3 0 00008
2 25544 51.6319 178.5071 0011018 103.7643 256.4573 15.48638586 07
| Epoch (UTC): | 16 February 2026 05:09:28 |
| Eccentricity: | 0.0011018 |
| inclination: | 51.6319° |
| perigee height: | 413 km |
| apogee height: | 428 km |
| right ascension of ascending node: | 178.5071° |
| argument of perigee: | 103.7643° |
| revolutions per day: | 15.48638586 |
| mean anomaly at epoch: | 256.4573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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