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 54150U 26145.56263380 +.00000000 +00000-0 +34419-3 0 00003
2 54150 82.5082 2.3568 0020517 271.6823 88.1906 12.42889909 04
| Epoch (UTC): | 25 May 2026 13:30:11 |
| Eccentricity: | 0.0020517 |
| inclination: | 82.5082° |
| perigee height: | 1478 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 2.3568° |
| argument of perigee: | 271.6823° |
| revolutions per day: | 12.42889909 |
| mean anomaly at epoch: | 88.1906° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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