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 61898U 26145.63724292 +.00000000 +00000-0 +46211-3 0 00005
2 61898 97.4121 216.9828 0058104 80.5386 280.2405 15.10654050 00
| Epoch (UTC): | 25 May 2026 15:17:37 |
| Eccentricity: | 0.0058104 |
| inclination: | 97.4121° |
| perigee height: | 494 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 216.9828° |
| argument of perigee: | 80.5386° |
| revolutions per day: | 15.10654050 |
| mean anomaly at epoch: | 280.2405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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