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 05118U 26041.52269027 +.00000000 +00000-0 +41442-3 0 00002
2 05118 81.2346 85.5321 0017282 30.4059 329.8191 15.58952925 00
| Epoch (UTC): | 10 February 2026 12:32:40 |
| Eccentricity: | 0.0017282 |
| inclination: | 81.2346° |
| perigee height: | 379 km |
| apogee height: | 402 km |
| right ascension of ascending node: | 85.5321° |
| argument of perigee: | 30.4059° |
| revolutions per day: | 15.58952925 |
| mean anomaly at epoch: | 329.8191° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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