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 63693U 26145.60946715 +.00000000 +00000-0 +84198-4 0 00000
2 63693 86.5063 320.8085 0001293 74.0542 286.0734 13.24406776 00
| Epoch (UTC): | 25 May 2026 14:37:37 |
| Eccentricity: | 0.0001293 |
| inclination: | 86.5063° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 320.8085° |
| argument of perigee: | 74.0542° |
| revolutions per day: | 13.24406776 |
| mean anomaly at epoch: | 286.0734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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