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 00082U 26046.16965207 +.00000000 +00000-0 +22685-3 0 00003
2 00082 38.8568 93.0111 1167188 355.3171 3.7349 12.27858533 02
| Epoch (UTC): | 15 February 2026 04:04:17 |
| Eccentricity: | 0.1167188 |
| inclination: | 38.8568° |
| perigee height: | 632 km |
| apogee height: | 2485 km |
| right ascension of ascending node: | 93.0111° |
| argument of perigee: | 355.3171° |
| revolutions per day: | 12.27858533 |
| mean anomaly at epoch: | 3.7349° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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