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 53840U 26145.48100065 +.00000000 +00000-0 -69849-4 0 00006
2 53840 53.2123 309.4499 0001636 91.9069 268.2111 15.08839186 06
| Epoch (UTC): | 25 May 2026 11:32:38 |
| Eccentricity: | 0.0001636 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 309.4499° |
| argument of perigee: | 91.9069° |
| revolutions per day: | 15.08839186 |
| mean anomaly at epoch: | 268.2111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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