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 63672U 26145.38386922 +.00000000 +00000-0 +14218-2 0 00004
2 63672 43.0024 176.1446 0000551 201.8080 158.2765 15.70946160 01
| Epoch (UTC): | 25 May 2026 09:12:46 |
| Eccentricity: | 0.0000551 |
| inclination: | 43.0024° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 176.1446° |
| argument of perigee: | 201.8080° |
| revolutions per day: | 15.70946160 |
| mean anomaly at epoch: | 158.2765° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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