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 61897U 26145.65074567 +.00000000 +00000-0 +28737-3 0 00002
2 61897 97.4102 217.6058 0013547 132.3856 227.8527 15.17713767 01
| Epoch (UTC): | 25 May 2026 15:37:04 |
| Eccentricity: | 0.0013547 |
| inclination: | 97.4102° |
| perigee height: | 503 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 217.6058° |
| argument of perigee: | 132.3856° |
| revolutions per day: | 15.17713767 |
| mean anomaly at epoch: | 227.8527° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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