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 26049.21532624 +.00000000 +00000-0 +18044-3 0 00009
2 25544 51.6322 168.6154 0010954 110.1068 250.1100 15.48678459 04
| Epoch (UTC): | 18 February 2026 05:10:04 |
| Eccentricity: | 0.0010954 |
| inclination: | 51.6322° |
| perigee height: | 413 km |
| apogee height: | 428 km |
| right ascension of ascending node: | 168.6154° |
| argument of perigee: | 110.1068° |
| revolutions per day: | 15.48678459 |
| mean anomaly at epoch: | 250.1100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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