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 26145.62932822 +.00000000 +00000-0 +18421-3 0 00009
2 44881 97.7531 218.4114 0014094 155.3218 204.8676 14.86477687 04
| Epoch (UTC): | 25 May 2026 15:06:13 |
| Eccentricity: | 0.0014094 |
| inclination: | 97.7531° |
| perigee height: | 599 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 218.4114° |
| argument of perigee: | 155.3218° |
| revolutions per day: | 14.86477687 |
| mean anomaly at epoch: | 204.8676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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