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 26042.18139057 +.00000000 +00000-0 +22024-3 0 00004
2 25544 51.6314 203.3958 0011074 86.6860 273.5395 15.48540110 02
| Epoch (UTC): | 11 February 2026 04:21:12 |
| Eccentricity: | 0.0011074 |
| inclination: | 51.6314° |
| perigee height: | 413 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 203.3958° |
| argument of perigee: | 86.6860° |
| revolutions per day: | 15.48540110 |
| mean anomaly at epoch: | 273.5395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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