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 63992U 26142.58614161 +.00000000 +00000-0 +51875-3 0 00008
2 63992 97.3665 216.1083 0011444 46.1259 314.0919 15.20032467 06
| Epoch (UTC): | 22 May 2026 14:04:02 |
| Eccentricity: | 0.0011444 |
| inclination: | 97.3665° |
| perigee height: | 498 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 216.1083° |
| argument of perigee: | 46.1259° |
| revolutions per day: | 15.20032467 |
| mean anomaly at epoch: | 314.0919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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