DUMMY SAT 3 is a payload in GEO orbit, operated by Khrunichev State Research and Production Center, launched 2024.
| Orbit class | GEO |
| Inclination | 2.1776° |
| Eccentricity | 0.0051636 |
| Period | 1460.4 min |
| Apogee | 36,480 km |
| Perigee | 36,040 km |
| Mean motion | 0.98605662 rev/day |
| RAAN | 81.2156° |
| Arg of perigee | 134.7734° |
| Mean anomaly | 225.2798° |
| B* | 0.0000e+0 |
| Rev at epoch | 800 |
1 59479U 24069A 26187.69010350 .00000012 00000-0 00000-0 0 99962 59479 2.1776 81.2156 0051636 134.7734 225.2798 0.98605662 8007{
"OBJECT_NAME": "DUMMY SAT 3",
"OBJECT_ID": "2024-069A",
"EPOCH": "2026-07-06T16:33:44.942+00:00",
"MEAN_MOTION": 0.98605662,
"ECCENTRICITY": 0.0051636,
"INCLINATION": 2.1776,
"RA_OF_ASC_NODE": 81.2156,
"ARG_OF_PERICENTER": 134.7734,
"MEAN_ANOMALY": 225.2798,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 59479,
"REV_AT_EPOCH": 800,
"BSTAR": 0,
"MEAN_MOTION_DOT": 1.2e-7,
"MEAN_MOTION_DDOT": 0
}Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.
| Name | DUMMY SAT 3 |
| Operator | |
| Country | Russia |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class | PAYLOADHIGH |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |