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 63701U 26145.58335647 +.00000000 +00000-0 +16482-2 0 00002
2 63701 53.1602 222.5211 0001403 60.9355 190.6953 15.31716590 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001403 |
| inclination: | 53.1602° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 222.5211° |
| argument of perigee: | 60.9355° |
| revolutions per day: | 15.31716590 |
| mean anomaly at epoch: | 190.6953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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