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 61227U 26145.63611727 +.00000000 +00000-0 +85573-3 0 00003
2 61227 97.3403 232.4683 0002354 296.5174 63.5845 15.66096402 02
| Epoch (UTC): | 25 May 2026 15:16:00 |
| Eccentricity: | 0.0002354 |
| inclination: | 97.3403° |
| perigee height: | 368 km |
| apogee height: | 372 km |
| right ascension of ascending node: | 232.4683° |
| argument of perigee: | 296.5174° |
| revolutions per day: | 15.66096402 |
| mean anomaly at epoch: | 63.5845° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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