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 61900U 26145.63495296 +.00000000 +00000-0 +34157-3 0 00004
2 61900 97.4135 216.1980 0018460 222.5454 137.4346 15.10409386 02
| Epoch (UTC): | 25 May 2026 15:14:19 |
| Eccentricity: | 0.0018460 |
| inclination: | 97.4135° |
| perigee height: | 522 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 216.1980° |
| argument of perigee: | 222.5454° |
| revolutions per day: | 15.10409386 |
| mean anomaly at epoch: | 137.4346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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