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 54672U 26145.57538125 +.00000000 +00000-0 +81507-4 0 00006
2 54672 87.9263 248.4639 0002503 98.1505 261.9913 13.21824691 03
| Epoch (UTC): | 25 May 2026 13:48:32 |
| Eccentricity: | 0.0002503 |
| inclination: | 87.9263° |
| perigee height: | 1176 km |
| apogee height: | 1180 km |
| right ascension of ascending node: | 248.4639° |
| argument of perigee: | 98.1505° |
| revolutions per day: | 13.21824691 |
| mean anomaly at epoch: | 261.9913° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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