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 26038.32328844 +.00000000 +00000-0 +13542-3 0 00009
2 44881 97.7668 113.6719 0014212 148.8785 211.3276 14.86269656 04
| Epoch (UTC): | 07 February 2026 07:45:32 |
| Eccentricity: | 0.0014212 |
| inclination: | 97.7668° |
| perigee height: | 600 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 113.6719° |
| argument of perigee: | 148.8785° |
| revolutions per day: | 14.86269656 |
| mean anomaly at epoch: | 211.3276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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