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 25413U 26087.98657558 +.00000000 +00000-0 +33458-3 0 00000
2 25413 44.9959 352.7778 0001666 222.6571 137.4147 14.35781638 03
| Epoch (UTC): | 28 March 2026 23:40:40 |
| Eccentricity: | 0.0001666 |
| inclination: | 44.9959° |
| perigee height: | 771 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 352.7778° |
| argument of perigee: | 222.6571° |
| revolutions per day: | 14.35781638 |
| mean anomaly at epoch: | 137.4147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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