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 41456U 26150.50579946 +.00000000 +00000-0 +27148-3 0 00007
2 41456 98.0920 210.5812 0016811 184.3903 175.7174 14.99112252 02
| Epoch (UTC): | 30 May 2026 12:08:21 |
| Eccentricity: | 0.0016811 |
| inclination: | 98.0920° |
| perigee height: | 558 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 210.5812° |
| argument of perigee: | 184.3903° |
| revolutions per day: | 14.99112252 |
| mean anomaly at epoch: | 175.7174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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