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 28155U 26070.15176212 +.00000000 +00000-0 +18797-2 0 00008
2 28155 12.7314 322.8819 6211093 184.6353 164.4954 3.70552371 02
| Epoch (UTC): | 11 March 2026 03:38:32 |
| Eccentricity: | 0.6211093 |
| inclination: | 12.7314° |
| perigee height: | 306 km |
| apogee height: | 22218 km |
| right ascension of ascending node: | 322.8819° |
| argument of perigee: | 184.6353° |
| revolutions per day: | 3.70552371 |
| mean anomaly at epoch: | 164.4954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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