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 00012U 26049.03283272 +.00000000 +00000-0 +33902-3 0 00004
2 00012 32.9020 285.1727 1646893 194.1384 160.7073 11.48538884 04
| Epoch (UTC): | 18 February 2026 00:47:16 |
| Eccentricity: | 0.1646893 |
| inclination: | 32.9020° |
| perigee height: | 553 km |
| apogee height: | 3286 km |
| right ascension of ascending node: | 285.1727° |
| argument of perigee: | 194.1384° |
| revolutions per day: | 11.48538884 |
| mean anomaly at epoch: | 160.7073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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