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 65673U 26145.55643000 +.00000000 +00000-0 +22650-3 0 00009
2 65673 97.4465 189.5447 0001613 117.9571 242.1820 15.05655591 05
| Epoch (UTC): | 25 May 2026 13:21:15 |
| Eccentricity: | 0.0001613 |
| inclination: | 97.4465° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 189.5447° |
| argument of perigee: | 117.9571° |
| revolutions per day: | 15.05655591 |
| mean anomaly at epoch: | 242.1820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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