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 15378U 26037.00197209 +.00000000 +00000-0 +23468-4 0 00000
2 15378 64.9922 40.9311 0036526 12.8465 347.3517 13.83704413 08
| Epoch (UTC): | 06 February 2026 00:02:50 |
| Eccentricity: | 0.0036526 |
| inclination: | 64.9922° |
| perigee height: | 924 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 40.9311° |
| argument of perigee: | 12.8465° |
| revolutions per day: | 13.83704413 |
| mean anomaly at epoch: | 347.3517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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