▸Orbital parameters

Orbit class	SSO
Inclination	97.4414°
Eccentricity	0.0001724
Period	94.8 min
Apogee	508 km
Perigee	506 km
Mean motion	15.19735624 rev/day
RAAN	31.3525°
Arg of perigee	90.6945°
Mean anomaly	269.4487°
B*	1.4560e-4
Rev at epoch	8,874

▸Two-line element set (TLE)

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

1 62138U 24223A 26188.19532259 .00003043 00000-0 14560-3 0 9993

2 62138 97.4414 31.3525 0001724 90.6945 269.4487 15.19735624 88747

▸ source OMM (JSON)

{
  "OBJECT_NAME": "KONDOR-FKA NO. 2",
  "OBJECT_ID": "2024-223A",
  "EPOCH": "2026-07-07T04:41:15.872+00:00",
  "MEAN_MOTION": 15.19735624,
  "ECCENTRICITY": 0.0001724,
  "INCLINATION": 97.4414,
  "RA_OF_ASC_NODE": 31.3525,
  "ARG_OF_PERICENTER": 90.6945,
  "MEAN_ANOMALY": 269.4487,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62138,
  "REV_AT_EPOCH": 8874,
  "BSTAR": 0.0001456,
  "MEAN_MOTION_DOT": 0.00003043,
  "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	KONDOR-FKA NO. 2
Operator	NPO MashinostroenieHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Nov 29, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	1050HIGHvia 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/62138

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