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 42828U 26150.40501794 +.00000000 +00000-0 +64810-3 0 00003
2 42828 97.4025 324.1340 0011074 112.5064 247.7346 15.21528649 08
| Epoch (UTC): | 30 May 2026 09:43:13 |
| Eccentricity: | 0.0011074 |
| inclination: | 97.4025° |
| perigee height: | 494 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 324.1340° |
| argument of perigee: | 112.5064° |
| revolutions per day: | 15.21528649 |
| mean anomaly at epoch: | 247.7346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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