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 28738U 26071.59537205 +.00000000 +00000-0 +54090-3 0 00004
2 28738 97.3599 86.8489 0005369 39.5162 320.6486 15.60430671 06
| Epoch (UTC): | 12 March 2026 14:17:20 |
| Eccentricity: | 0.0005369 |
| inclination: | 97.3599° |
| perigee height: | 383 km |
| apogee height: | 390 km |
| right ascension of ascending node: | 86.8489° |
| argument of perigee: | 39.5162° |
| revolutions per day: | 15.60430671 |
| mean anomaly at epoch: | 320.6486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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