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 51657U 26121.68095022 +.00000000 +00000-0 +90138-3 0 00005
2 51657 97.4223 174.4124 0009835 243.9293 116.0991 16.33437437 01
| Epoch (UTC): | 01 May 2026 16:20:34 |
| Eccentricity: | 0.0009835 |
| inclination: | 97.4223° |
| perigee height: | 177 km |
| apogee height: | 190 km |
| right ascension of ascending node: | 174.4124° |
| argument of perigee: | 243.9293° |
| revolutions per day: | 16.33437437 |
| mean anomaly at epoch: | 116.0991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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