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 63088U 26145.38028709 +.00000000 +00000-0 +26062-3 0 00002
2 63088 70.0005 160.9284 0003963 266.7802 93.2904 14.98337463 06
| Epoch (UTC): | 25 May 2026 09:07:36 |
| Eccentricity: | 0.0003963 |
| inclination: | 70.0005° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 160.9284° |
| argument of perigee: | 266.7802° |
| revolutions per day: | 14.98337463 |
| mean anomaly at epoch: | 93.2904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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