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 51465U 26144.79876701 +.00000000 +00000-0 +37355-4 0 00003
2 51465 53.2142 297.4544 0001208 88.2921 271.8210 15.08840119 04
| Epoch (UTC): | 24 May 2026 19:10:13 |
| Eccentricity: | 0.0001208 |
| inclination: | 53.2142° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 297.4544° |
| argument of perigee: | 88.2921° |
| revolutions per day: | 15.08840119 |
| mean anomaly at epoch: | 271.8210° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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