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 44881U 26160.16913984 +.00000000 +00000-0 +17610-3 0 00002
2 44881 97.7528 232.5966 0014956 110.5394 249.7428 14.86509678 06
| Epoch (UTC): | 09 June 2026 04:03:33 |
| Eccentricity: | 0.0014956 |
| inclination: | 97.7528° |
| perigee height: | 598 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 232.5966° |
| argument of perigee: | 110.5394° |
| revolutions per day: | 14.86509678 |
| mean anomaly at epoch: | 249.7428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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