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 63797U 26145.53678728 +.00000000 +00000-0 +63921-3 0 00003
2 63797 43.0017 342.1768 0001108 297.5528 62.5211 15.27588147 03
| Epoch (UTC): | 25 May 2026 12:52:58 |
| Eccentricity: | 0.0001108 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 342.1768° |
| argument of perigee: | 297.5528° |
| revolutions per day: | 15.27588147 |
| mean anomaly at epoch: | 62.5211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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