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 51140U 26145.55965161 +.00000000 +00000-0 -12146-4 0 00009
2 51140 53.2129 314.0461 0001239 96.8016 263.3117 15.08832074 00
| Epoch (UTC): | 25 May 2026 13:25:53 |
| Eccentricity: | 0.0001239 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 314.0461° |
| argument of perigee: | 96.8016° |
| revolutions per day: | 15.08832074 |
| mean anomaly at epoch: | 263.3117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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