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 51995U 26145.38205260 +.00000000 +00000-0 -53262-4 0 00009
2 51995 53.2132 34.8333 0001546 86.4879 273.6290 15.08833630 05
| Epoch (UTC): | 25 May 2026 09:10:09 |
| Eccentricity: | 0.0001546 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 34.8333° |
| argument of perigee: | 86.4879° |
| revolutions per day: | 15.08833630 |
| mean anomaly at epoch: | 273.6290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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