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 63982U 26144.76158051 +.00000000 +00000-0 +19099-3 0 00002
2 63982 97.3675 218.0864 0030581 87.8153 272.6583 15.19876603 04
| Epoch (UTC): | 24 May 2026 18:16:40 |
| Eccentricity: | 0.0030581 |
| inclination: | 97.3675° |
| perigee height: | 485 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 218.0864° |
| argument of perigee: | 87.8153° |
| revolutions per day: | 15.19876603 |
| mean anomaly at epoch: | 272.6583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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