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 26088.19079089 +.00000000 +00000-0 +60879-4 0 00002
2 12988 82.5214 302.0676 0018257 45.2934 314.9766 14.87286218 09
| Epoch (UTC): | 29 March 2026 04:34:44 |
| Eccentricity: | 0.0018257 |
| inclination: | 82.5214° |
| perigee height: | 594 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 302.0676° |
| argument of perigee: | 45.2934° |
| revolutions per day: | 14.87286218 |
| mean anomaly at epoch: | 314.9766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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