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 54820U 26145.04597509 +.00000000 +00000-0 -74107-4 0 00003
2 54820 43.0044 64.6277 0001323 265.3151 94.7550 15.27579644 00
| Epoch (UTC): | 25 May 2026 01:06:12 |
| Eccentricity: | 0.0001323 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 64.6277° |
| argument of perigee: | 265.3151° |
| revolutions per day: | 15.27579644 |
| mean anomaly at epoch: | 94.7550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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