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 15370U 26044.71108252 +.00000000 +00000-0 +51223-4 0 00008
2 15370 82.5142 279.0400 0021379 54.8122 305.5092 14.86036489 09
| Epoch (UTC): | 13 February 2026 17:03:57 |
| Eccentricity: | 0.0021379 |
| inclination: | 82.5142° |
| perigee height: | 595 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 279.0400° |
| argument of perigee: | 54.8122° |
| revolutions per day: | 14.86036489 |
| mean anomaly at epoch: | 305.5092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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