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 63245U 26145.67194251 +.00000000 +00000-0 +19563-3 0 00003
2 63245 97.6898 37.1412 0002603 306.2228 53.8751 14.94531959 00
| Epoch (UTC): | 25 May 2026 16:07:35 |
| Eccentricity: | 0.0002603 |
| inclination: | 97.6898° |
| perigee height: | 582 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 37.1412° |
| argument of perigee: | 306.2228° |
| revolutions per day: | 14.94531959 |
| mean anomaly at epoch: | 53.8751° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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