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 26048.90368258 +.00000000 +00000-0 +57364-3 0 00000
2 00107 28.7754 283.9857 0495557 94.5097 271.2234 14.21544620 04
| Epoch (UTC): | 17 February 2026 21:41:18 |
| Eccentricity: | 0.0495557 |
| inclination: | 28.7754° |
| perigee height: | 463 km |
| apogee height: | 1177 km |
| right ascension of ascending node: | 283.9857° |
| argument of perigee: | 94.5097° |
| revolutions per day: | 14.21544620 |
| mean anomaly at epoch: | 271.2234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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