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 65998U 26145.29391352 +.00000000 +00000-0 +51740-4 0 00003
2 65998 49.9997 257.7992 0000940 151.1180 208.9744 13.29325708 01
| Epoch (UTC): | 25 May 2026 07:03:14 |
| Eccentricity: | 0.0000940 |
| inclination: | 49.9997° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 257.7992° |
| argument of perigee: | 151.1180° |
| revolutions per day: | 13.29325708 |
| mean anomaly at epoch: | 208.9744° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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