▸Orbital parameters

Orbit class	SSO
Inclination	97.8132°
Eccentricity	0.0011245
Period	95.6 min
Apogee	555 km
Perigee	540 km
Mean motion	15.06267198 rev/day
RAAN	325.1438°
Arg of perigee	2.4161°
Mean anomaly	357.7117°
B*	1.3956e-4
Rev at epoch	1,209

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 68759U 26083G 26187.47962785 .00001986 00000-0 13956-3 0 9997

2 68759 97.8132 325.1438 0011245 2.4161 357.7117 15.06267198 12098

▸ source OMM (JSON)

{
  "OBJECT_NAME": "COSMOS 2611",
  "OBJECT_ID": "2026-083G",
  "EPOCH": "2026-07-06T11:30:39.846+00:00",
  "MEAN_MOTION": 15.06267198,
  "ECCENTRICITY": 0.0011245,
  "INCLINATION": 97.8132,
  "RA_OF_ASC_NODE": 325.1438,
  "ARG_OF_PERICENTER": 2.4161,
  "MEAN_ANOMALY": 357.7117,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68759,
  "REV_AT_EPOCH": 1209,
  "BSTAR": 0.00013955989,
  "MEAN_MOTION_DOT": 0.00001986,
  "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.

▸Satellite metadata

Name	COSMOS 2611
Operator	Aerospace Defence ForcesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Apr 16, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	500HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/68759

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.