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 00107U 26049.95692291 +.00000000 +00000-0 +54408-3 0 00009
2 00107 28.7752 277.9172 0495492 104.3467 261.2617 14.21554251 09
| Epoch (UTC): | 18 February 2026 22:57:58 |
| Eccentricity: | 0.0495492 |
| inclination: | 28.7752° |
| perigee height: | 463 km |
| apogee height: | 1177 km |
| right ascension of ascending node: | 277.9172° |
| argument of perigee: | 104.3467° |
| revolutions per day: | 14.21554251 |
| mean anomaly at epoch: | 261.2617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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