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 12988U 26073.65863514 +.00000000 +00000-0 +58168-4 0 00009
2 12988 82.5245 315.7590 0018755 89.8122 270.5244 14.87273262 08
| Epoch (UTC): | 14 March 2026 15:48:26 |
| Eccentricity: | 0.0018755 |
| inclination: | 82.5245° |
| perigee height: | 593 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 315.7590° |
| argument of perigee: | 89.8122° |
| revolutions per day: | 14.87273262 |
| mean anomaly at epoch: | 270.5244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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