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 54666U 26145.51732860 +.00000000 +00000-0 +22790-3 0 00003
2 54666 87.9250 248.5122 0001972 91.9850 268.1510 13.21824814 02
| Epoch (UTC): | 25 May 2026 12:24:57 |
| Eccentricity: | 0.0001972 |
| inclination: | 87.9250° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.5122° |
| argument of perigee: | 91.9850° |
| revolutions per day: | 13.21824814 |
| mean anomaly at epoch: | 268.1510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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