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 63971U 26145.23769240 +.00000000 +00000-0 +51172-3 0 00009
2 63971 42.9984 100.4169 0001059 275.0513 85.0217 15.27592651 09
| Epoch (UTC): | 25 May 2026 05:42:16 |
| Eccentricity: | 0.0001059 |
| inclination: | 42.9984° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.4169° |
| argument of perigee: | 275.0513° |
| revolutions per day: | 15.27592651 |
| mean anomaly at epoch: | 85.0217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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