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 63284U 26145.52091081 +.00000000 +00000-0 -28403-3 0 00001
2 63284 43.0006 160.0832 0001876 272.1411 87.9226 15.27592904 06
| Epoch (UTC): | 25 May 2026 12:30:06 |
| Eccentricity: | 0.0001876 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 160.0832° |
| argument of perigee: | 272.1411° |
| revolutions per day: | 15.27592904 |
| mean anomaly at epoch: | 87.9226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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