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 63160U 26145.56527251 +.00000000 +00000-0 +13919-3 0 00006
2 63160 88.9690 302.9282 0001875 100.9231 259.2131 13.51004279 06
| Epoch (UTC): | 25 May 2026 13:33:59 |
| Eccentricity: | 0.0001875 |
| inclination: | 88.9690° |
| perigee height: | 1067 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 302.9282° |
| argument of perigee: | 100.9231° |
| revolutions per day: | 13.51004279 |
| mean anomaly at epoch: | 259.2131° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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