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 63197U 26145.34471781 +.00000000 +00000-0 +18403-2 0 00000
2 63197 43.0044 12.5796 0001796 268.0094 92.0552 15.27655575 06
| Epoch (UTC): | 25 May 2026 08:16:23 |
| Eccentricity: | 0.0001796 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 12.5796° |
| argument of perigee: | 268.0094° |
| revolutions per day: | 15.27655575 |
| mean anomaly at epoch: | 92.0552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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