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 63950U 26145.25402414 +.00000000 +00000-0 +25817-3 0 00002
2 63950 70.0009 81.3034 0002975 261.9737 98.1084 14.98337527 07
| Epoch (UTC): | 25 May 2026 06:05:47 |
| Eccentricity: | 0.0002975 |
| inclination: | 70.0009° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 81.3034° |
| argument of perigee: | 261.9737° |
| revolutions per day: | 14.98337527 |
| mean anomaly at epoch: | 98.1084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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