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 44874U 26145.49875231 +.00000000 +00000-0 +65241-4 0 00009
2 44874 98.1510 334.0845 0010832 163.9360 196.2187 14.61946440 05
| Epoch (UTC): | 25 May 2026 11:58:12 |
| Eccentricity: | 0.0010832 |
| inclination: | 98.1510° |
| perigee height: | 679 km |
| apogee height: | 695 km |
| right ascension of ascending node: | 334.0845° |
| argument of perigee: | 163.9360° |
| revolutions per day: | 14.61946440 |
| mean anomaly at epoch: | 196.2187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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