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 12987U 26064.24291586 +.00000000 +00000-0 +46130-3 0 00002
2 12987 82.4948 355.0266 0010276 183.8120 176.3046 15.33762384 09
| Epoch (UTC): | 05 March 2026 05:49:47 |
| Eccentricity: | 0.0010276 |
| inclination: | 82.4948° |
| perigee height: | 458 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 355.0266° |
| argument of perigee: | 183.8120° |
| revolutions per day: | 15.33762384 |
| mean anomaly at epoch: | 176.3046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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