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 53982U 26144.67779199 +.00000000 +00000-0 +37759-4 0 00007
2 53982 53.2136 233.0342 0001135 86.3248 273.7874 15.08836221 01
| Epoch (UTC): | 24 May 2026 16:16:01 |
| Eccentricity: | 0.0001135 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 233.0342° |
| argument of perigee: | 86.3248° |
| revolutions per day: | 15.08836221 |
| mean anomaly at epoch: | 273.7874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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