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 43897U 26040.42884448 +.00000000 +00000-0 +55435-3 0 00003
2 43897 96.9334 273.2764 0005120 253.9077 106.1660 16.39089821 06
| Epoch (UTC): | 09 February 2026 10:17:32 |
| Eccentricity: | 0.0005120 |
| inclination: | 96.9334° |
| perigee height: | 165 km |
| apogee height: | 172 km |
| right ascension of ascending node: | 273.2764° |
| argument of perigee: | 253.9077° |
| revolutions per day: | 16.39089821 |
| mean anomaly at epoch: | 106.1660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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